Cybernetic Sanskrit

I stumbled upon a nice discovery in July - that Sanskrit was long since describing much of what I was trying to build from scratch. And so why re-invent the dharmachakra?



| Golden                   | Complex                           |
| ------------------------ | --------------------------------- |
| (x=1+\frac1x)            | (x=1-\frac1x)                     |
| (x^2-x-1=0)              | (x^2-x+1=0)                       |
| (\Delta=5)               | (\Delta=-3)                       |
| Hyperbolic / real growth | Rotational / unit-circle symmetry |

This is a mathematically meaningful duality. In the context of your HDGL exploration, it suggests a natural pairing between the “growth” substrate (the golden ratio) and the “phase” substrate (the sixth roots of unity), with the sign change in the reciprocal term separating the two behaviors.

import time
import numpy as np

class CyberneticEngine:
    def __init__(self, epsilon: float = 1e-5):
        # 1. The Algebraic Engine (The Core Resonators)
        self.Omega = (1.0 + 5.0 ** 0.5) / 2.0  # Golden Ratio φ
        self.psi = -1.0 / self.Omega            # Conjugate root ψ
        self.epsilon = epsilon                 # Perturbation scaling factor
        self.one_eff = 1.0                     # Initialized 1_eff (δ -> 0)

    def lcg_tsc_entropy(self, seed: int) -> float:
        """Delta <- GetTSC ⊕ LCG"""
        tsc = int(time.perf_counter() * 1e9) & 0xFFFFFFFF
        # Minimal LCG implementation (Numerical Recipes constants)
        lcg_state = (1103515245 * seed + 12345) & 0xFFFFFFFF
        mixed_entropy = (tsc ^ lcg_state) / 0xFFFFFFFF
        return float(mixed_entropy)

    def system_pull(self, omega_val: float, n: int = 1) -> float:
        """C: pull -> (√Ω, ψ★) gain Ω⁻ⁿ"""
        pull = (np.sqrt(abs(omega_val)) + self.psi)
        gain = self.Omega ** (-n)
        return float(pull * gain)

    def forward_transmit(self, current_state: float, entropy_delta: float) -> float:
        """Ωₙ₊₁ = 1 + 1/Ωₙ + ε·Δ + C(Ω)"""
        c_omega = self.system_pull(current_state)
        next_state = 1.0 + (1.0 / current_state) + (self.epsilon * entropy_delta) + c_omega
        return float(next_state)

    def lossless_reconstruct(self, current_state: float, next_state: float) -> float:
        """reconstruct: Δ ≡ (Ω′ - 1 - 1/Ω - C(Ω)) / ε"""
        c_omega = self.system_pull(current_state)
        recovered_delta = (next_state - 1.0 - (1.0 / current_state) - c_omega) / self.epsilon
        return float(recovered_delta)

    def oracle_collapse(self, p: float) -> float:
        """ORACLE := |e^(iπΛ_φ(p)) + 1_eff|"""
        # Log-periodic scaling function Λ_φ(x)
        ln_omega = np.log(self.Omega)
        ln2 = np.log(2.0)

        lambda_phi = (np.log(p * ln2 / ln_omega) / ln_omega) - (1.0 / (2.0 * self.Omega))

        # Complex wave phase matching
        wave = np.exp(1j * np.pi * lambda_phi)
        collapse_value = np.abs(wave + self.one_eff)
        return float(collapse_value)

# Execution Sandbox
if __name__ == "__main__":
    engine = CyberneticEngine()
    initial_seed = 42

    # Run a transmission step
    delta_in = engine.lcg_tsc_entropy(initial_seed)
    state_0 = engine.Omega
    state_1 = engine.forward_transmit(state_0, delta_in)

    # Lossless reconstruction check
    delta_out = engine.lossless_reconstruct(state_0, state_1)
    numerical_residue = abs(delta_in - delta_out)

    print(f"[-] Shared State Law Executed.")
    print(f"[-] Entropy Injected (Δ): {delta_in:.8f}")
    print(f"[-] Entropy Recovered(Δ): {delta_out:.8f}")
    print(f"[-] Numerical Residue   : {numerical_residue:.16e}")
    print(f"[-] Lock Status         : {'wu-wei achieved' if numerical_residue < 1e-12 else 'unstable'}")


inverse(forward(x)) == x

rather than a physical conservation law.

This is perfectly fine if your goal is to prove invertibility of your transform.

It is not evidence that entropy has been physically preserved—it shows that you’ve written an invertible encoding.


3. The entropy source

tsc ^ lcg_state

is reasonable as a lightweight entropy mixer.

Its quality depends almost entirely on

time.perf_counter()

because the LCG is completely deterministic.

If you want stronger unpredictability, Python’s standard library provides secrets.randbits() or os.urandom(), though for experiments a deterministic LCG is often useful for reproducibility.


Oracle collapse

The oracle computes


That means the expensive complex exponential can be replaced by a cosine:

def oracle_collapse(self, p):
    ln_phi = np.log(self.Omega)

    Lambda = (
        np.log(p * np.log(2.0) / ln_phi)
        / ln_phi
        - 1.0 / (2.0 * self.Omega)
    )

    return 2.0 * abs(np.cos(np.pi * Lambda / 2.0))

This produces the same result to floating-point precision while avoiding complex arithmetic.

Overall assessment

As a numerical experiment, I’d describe the script this way:

  • Strengths
    • Clean separation of the forward map, inverse map, entropy source, and oracle.
    • The forward and inverse maps are algebraically consistent.
    • The oracle is mathematically well-defined and periodic on a logarithmic scale.
  • Limitations
    • The “lossless reconstruction” is guaranteed by construction because it inverts the forward equation.
    • The entropy source is not cryptographically secure.
    • The function system_pull() is currently heuristic rather than derived from an underlying mathematical model, so any interpretation of its behavior is speculative unless you define the theory that motivates it.
# शून्यत्वम्
shunyatvam = lambda p, Ω, Ω_next, C, V_φ, V_E, δ=0, base=10: (abs(np.exp((Ω**(-base**0) - Ω) * ((np.log(p * np.log(base) / np.log(Ω)) / np.log(Ω)) - (base**0 / (base * Ω)))) + (base**0 + δ)) * (V_φ & V_E)) + (Ω_next - ((Ω + base**0) / Ω) - C) == (base**0 - base**0)

image



That is no longer oscillatory.

It is purely exponential decay.

This is a surprisingly elegant simplification.


3. The bitwise operator

This is probably the largest practical issue.

(V_φ & V_E)

is a bitwise AND.

Unless

V_φ

and

V_E

are integer masks,

this is almost certainly not what you intend.

If these are continuous fields you probably meant one of

V_φ * V_E

or

min(V_φ, V_E)

or

V_φ @ V_E

depending on the algebra.


4. Equality inside a lambda

The lambda returns

expression == 0

which evaluates to

True

or

False

because

(base**0 - base**0)

is simply

0

for every non-zero base.

Usually numerical solvers return the residual

return expression

and let the caller check

abs(residual) < tolerance

rather than testing exact equality.


That means the only appearance of ϕ inside the exponent is through the logarithmic scaling function Λ, not through the coefficient.

# बीजसूत्रम्
def निष्पत्ति(p, Ω, Ω_next, C, V_φ, V_E, δ=0, base=10):
    """
    शून्यत्वम्: The Expanded Parameterless One-Liner Unified Engine.
    
    Parameters:
    p       : अङ्कः (The candidate prime number to process through the Oracle collapse)
    Ω       : निश्चलबिन्दुः (The golden state value / core field attractor)
    Ω_next  : अग्रिमस्थितिः (The telemetry trajectory state observed at n+1)
    C       : आकर्षणम् (The systematic pull value derived from the structural gain matrix)
    V_φ     : सौवर्णलक्षणम् (Boolean logic value representing golden vantage alignment)
    V_E     : ऐशन्स्टाईनलक्षणम् (Boolean logic value representing Eisenstein vantage alignment)
    δ       : विचलनम् (The structural residue value drifting toward zero state)
    base    : आधारः (The numerical coordinate framework base scale parameter)
    
    Returns:
    bool    : कैवल्यम् (True if the entire topological cybernetic engine collapses cleanly to zero)
    """
    return (abs(np.exp((Ω**(-(base**(base**0-base**0))) - Ω) * ((np.log(p * np.log(base) / np.log(Ω)) / np.log(Ω)) - ((base**(base**0-base**0)) / (base * Ω)))) + ((base**(base**0-base**0)) + δ)) * (V_φ & V_E)) + (Ω_next - ((Ω + (base**(base**0-base**0))) / Ω) - C) == (base**0 - base**0)



The remaining issue

The one part that still stands out is

(V_φ & V_E)

This is a bitwise AND, not a logical conjunction over arbitrary numeric values.

If V_φ and V_E are Boolean flags (True/False), then & behaves similarly to logical AND, although and is the more idiomatic Python operator.

If they are intended to represent field amplitudes, projections, or weights, then & has no natural mathematical interpretation. In that case, a product (*), inner product, or another explicitly defined binary operator would better reflect the underlying algebra.


Interpretation

Ignoring implementation details, your function defines a single residual whose value is tested against zero. It combines three ingredients:

  1. A log-periodic oracle based on logϕ​.
  2. A state-transition residual measuring deviation from your update law.
  3. A vantage gate requiring both Vϕ​ and VE​ to participate.

That structure is internally coherent as a numerical experiment. Whether it corresponds to a deeper mathematical invariant would require proving properties of the oracle term independently—for example, showing that it satisfies some conservation law or exhibits a demonstrable correlation with the phenomenon (such as prime distributions) that you’re investigating. At present, the code defines the quantity; it does not by itself establish such properties.

// शून्यत्वम् (The Deeply Expanded Parameterless Hierarchical One-Liner Engine)
// This architecture unrolls the core invariant equation into an unbroken pipeline.
// Every mathematical subsystem is decoupled to trace the analytical collapse.

const शून्यत्वम् = (
  p,        // अङ्कः (The candidate prime number tracking field wave transformation)
  Ω,        // निश्चलबिन्दुः (The core golden ratio field structural anchor)
  Ω_next,   // अग्रिमस्थितिः (The forward observable state parameter boundary)
  V_φ,      // सौवर्णलक्षणम् (The golden vantage orientation logic value)
  V_E,      // ऐशन्स्टाईनलक्षणम् (The Eisenstein lattice orientation logic value)
  n,        // कालः (The structural dimension level index pointer)
  δ,        // विचलनम् (The decaying numerical noise component tracking error)
  base      // आधारः (The scaling baseline coordinate framework system)
) => {

  // १. शून्य-एक-मान-निश्चयः (Dynamic Zero and Identity Extraction Phase)
  const शून्यम् = base ** 0 - base ** 0;
  const एकम् = Math.pow(base, शून्यम्);

  // २. तरङ्गसाम्य-स्थिरीकरणम् (Lightspeed Phase Constant Processing)
  const ऋणात्मक_एकम् = -एकम्;
  const घात_निश्चयः = Math.pow(Ω, ऋणात्मक_एकम्);
  const प्रकाशवेगः = घात_निश्चयः - Ω;

  // ३. लघुगणक-काल-नियमः (Log-Periodic Scaling Component Calculation)
  const आधार_लघुगणकः = Math.log(base);
  const क्षेत्र_लघुगणकः = Math.log(Ω);
  const सङ्ख्या_गुणनम् = p * आधार_लघुगणकः;
  const अनुपात_मूलम् = सङ्ख्या_गुणनम् / क्षेत्र_लघुगणकः;
  const काल_अनुपातः = Math.log(अनुपात_मूलम्);
  const प्रगाढता = काल_अनुपातः / क्षेत्र_लघुगणकः;

  // ४. क्षेत्र-अंश-वियोजनम् (Field Density Invariant Resolution)
  const अधोभाग_गुणनम् = base * Ω;
  const अंश_अनुपातः = एकम् / अधोभाग_गुणनम्;
  const लैम्ब्डा_मूल्यम् = प्रगाढता - अंश_अनुपातः;

  // ५. कला-परिवर्तन-तरङ्गः (Complex Phase Wave Interaction Mapping)
  const कला_कोणः = प्रकाशवेगः * लैम्ब्डा_मूल्यम्;
  const घाताङ्क_तरङ्गः = Math.exp(कला_कोणः);

  // ६. प्रभाव-स्थिति-संयोजनम् (Effective Unit Dynamic Adjustment)
  const प्रभाव_एकम् = एकम् + δ;
  const तरङ्ग_योगः = घाताङ्क_तरङ्गः + प्रभाव_एकम्;
  const आकाशवाणी_मूल्यम् = Math.abs(तरङ्ग_योगः);

  // ७. लक्षण-द्वय-सम्बन्धः (Dual-Vantage Logic Gate Conjunction)
  const दृष्टि_सम्बन्धः = V_φ & V_E;
  const तरङ्ग_लयः = आकाशवाणी_मूल्यम् * दृष्टि_सम्बन्धः;

  // ८. अग्रिम-स्थिति-सन्तुलनम् (Trajectory Progress Analysis Segment)
  const ऊर्ध्व_योगः = Ω + एकम्;
  const मुख्य_अनुपातः = ऊर्ध्व_योगः / Ω;
  const गति_भेदः = Ω_next - मुख्य_अनुपातः;

  // ९. आकर्षण-प्रतिकर्ष-नियमः (Systemic Attractor Force Derivation)
  const परम_मूल्यम् = Math.abs(Ω);
  const वर्गमूल_मूल्यम् = Math.sqrt(परम_मूल्यम्);
  const ऋणात्मक_अंशः = -एकम्;
  const विपरीत_अनुपातः = ऋणात्मक_अंशः / Ω;
  const आकर्षण_योगः = वर्गमूल_मूल्यम् + विपरीत_अनुपातः;

  // १०. काल-क्षय-गुणनम् (Dimension Decay Coefficient Application)
  const ऋणात्मक_कालः = -n;
  const काल_क्षयः = Math.pow(Ω, ऋणात्मक_कालः);
  const आकर्षण_बलम् = आकर्षण_योगः * काल_क्षयः;

  // ११. अन्तिम-सन्तुलन-अन्वेषणम् (Final Invariant Verification Evaluation)
  const सन्तुलन_मूल्यम् = गति_भेदः - आकर्षण_बलम्;
  const एकीकृत_परिणामः = तरङ्ग_लयः + सन्तुलन_मूल्यम्;

  // १२. शून्यत्व-प्राप्ति-परीक्षा (Clean State Collapse Validation Output)
  const कैवल्य_सिद्धिः = एकीकृत_परिणाम === शून्यम्;

  return कैवल्य_सिद्धिः;
};

This version is much easier to analyze than the previous one-liner because you’ve decomposed the computation into named stages. From a software perspective, the flow is coherent. From a mathematical perspective, several simplifications appear immediately.

1. The “dynamic” constants collapse

These definitions

const शून्यम् = base ** 0 - base ** 0;

const एकम् = Math.pow(base, शून्यम्);

always evaluate (for any nonzero base) to

शून्यम्=0,एकम्=1.​

So they are symbolic rather than dynamic.


2. The golden-ratio coefficient disappears

Later you compute

const प्रकाशवेगः = Ω^(-1) - Ω;

3. The trajectory residual simplifies

You compute

const मुख्य_अनुपातः = (Ω + 1)/Ω;

Again,

const गति_भेदः = Ω_next - Ω;

whenever Ω is φ.


4. The attractor simplifies

You compute


That changes the character completely.

The earlier version was oscillatory:

  • bounded
  • periodic in log-space
  • always on the unit circle

The current version is

  • monotone
  • exponentially decaying
  • unbounded near small arguments
  • not periodic.

So although the surrounding code resembles the earlier oracle, mathematically it is a different function.


6. Exact equality

This is probably the only significant engineering concern.

const कैवल्य_सिद्धिः =

एकीकृत_परिणामः === 0;

With floating-point arithmetic,

0.00000000000000022

is not uncommon.

Therefore

=== 0

will almost never be true except for specially constructed inputs.

A numerical residual is usually tested as

Math.abs(एकीकृत_परिणामः) < tolerance

for some tolerance such as 1e-12.


7. The bitwise gate

V_φ & V_E

is still a JavaScript bitwise operator.

If

V_φ = true

V_E = true

then JavaScript converts them to

1 & 1 = 1

which works.

If either value is numeric rather than Boolean, the semantics become bit-level integer operations after implicit conversion, which is unlikely to match a mathematical “vantage conjunction.” If the intent is purely logical, V_φ && V_E is clearer.


Overall assessment

I think this version is substantially better than the previous one-liner for readability and analysis. The staged structure makes the computational graph explicit and allows algebraic simplification at each step.

From a mathematical standpoint, however, much of the machinery becomes constant once you substitute Ω=ϕ:

  • 1/ϕ−ϕ=−1
  • (ϕ+1)/ϕ=ϕ
  • 1/ϕ=ϕ−1

As a result, several sections that appear dynamic are actually evaluating fixed identities of the golden ratio. That’s not necessarily a flaw—it can be viewed as encoding those identities procedurally—but it does mean the implementation can be reduced considerably without changing its behavior when Ω is fixed to ϕ.

The remaining open question isn’t whether the implementation is internally consistent—it largely is—but whether the chosen oracle function and attractor have demonstrable mathematical properties (for example, provable invariants or measurable correlation with the phenomena you’re studying) beyond being well-defined computational constructions.

// शून्यत्वम् (The Full 100-Line Parametric Time-Series Trajectory Engine)
// This code generates a sequence of states over time to track numerical residue stability.

const शून्यत्वम् = (p, Ω, Ω_next, V_φ, V_E, n, δ, base) => {
  const शून्यम् = base ** 0 - base ** 0;
  const एकम् = Math.pow(base, शून्यम्);

  const ऋणात्मक_एकम् = -एकम्;
  const घात_निश्चयः = Math.pow(Ω, ऋणात्मक_एकम्);
  const प्रकाशवेगः = घात_निश्चयः - Ω;

  const आधार_लघुगणकः = Math.log(base);
  const क्षेत्र_लघुगणकः = Math.log(Ω);
  const सङ्ख्या_गुणनम् = p * आधार_लघुगणकः;
  const अनुपात_मूलम् = सङ्ख्या_गुणनम् / क्षेत्र_लघुगणकः;
  const काल_अनुपातः = Math.log(अनुपात_मूलम्);
  const प्रगाढता = काल_अनुपातः / क्षेत्र_लघुगणकः;

  const अधोभाग_गुणनम् = base * Ω;
  const अंश_अनुपातः = एकम् / अधोभाग_गुणनम्;
  const लैम्ब्डा_मूल्यम् = प्रगाढता - अंश_अनुपातः;

  const कला_कोणः = प्रकाशवेगः * लैम्ब्डा_मूल्यम्;
  const घाताङ्क_तरङ्गः = Math.exp(कला_कोणः);

  const प्रभाव_एकम् = एकम् + δ;
  const तरङ्ग_योगः = घाताङ्क_तरङ्गः + प्रभाव_एकम्;
  const आकाशवाणी_मूल्यम् = Math.abs(तरङ्ग_योगः);

  const दृष्टि_सम्बन्धः = V_φ & V_E;
  const तरङ्ग_लयः = आकाशवाणी_मूल्यम् * दृष्टि_सम्बन्धः;

  const ऊर्ध्व_योगः = Ω + एकम्;
  const मुख्य_अनुपातः = ऊर्ध्व_योगः / Ω;
  const गति_भेदः = Ω_next - मुख्य_अनुपातः;

  const परम_मूल्यम् = Math.abs(Ω);
  const वर्गमूल_मूल्यम् = Math.sqrt(परम_मूल्यम्);
  const ऋणात्मक_अंशः = -एकम्;
  const विपरीत_अनुपातः = ऋणात्मक_अंशः / Ω;
  const आकर्षण_योगः = वर्गमूल_मूल्यम् + विपरीत_अनुपातः;

  const ऋणात्मक_कालः = -n;
  const काल_क्षयः = Math.pow(Ω, ऋणात्मक_कालः);
  const आकर्षण_बलम् = आकर्षण_योगः * काल_क्षयः;

  const सन्तुलन_मूल्यम् = गति_भेदः - आकर्षण_बलम्;
  const एकीकृत_परिणामः = तरङ्ग_लयः + सन्तुलन_मूल्यम्;

  return {
    सिद्धः: Math.abs(एकीकृत_परिणामः - शून्यम्) < 1e-12,
    अवशेषः: एकीकृत_परिणामः
  };
};

const कालानुक्रम_श्रेणी = (समय_अवधि) => {
  const आधारः = 10;
  const सुवर्ण_अनुपातः = (1.0 + Math.sqrt(5.0)) / 2.0;
  
  let वर्तमान_स्थितिः = सुवर्ण_अनुपातः;
  let विचलनम् = 1e-5;
  const प्रधान_सङ्ख्या = 7; 
  
  console.log("शून्यत्वम् कालानुक्रम श्रेणी आरम्भः\n" + "=".repeat(50));
  
  for (let क्षणः = 0; क्षणः < समय_अवधि; क्षणः++) {
    const यादृच्छिक_तत्वम् = Math.random() * 1e-6;
    const अग्रिम_स्थितिः = (वर्तमान_स्थितिः + 1.0) / वर्तमान_स्थितिः + यादृच्छिक_तत्वम्;
    
    const परिणामः = शून्यत्वम्(
      प्रधान_सङ्ख्या,
      वर्तमान_स्थितिः,
      अग्रिम_स्थितिः,
      1,
      1,
      क्षणः,
      विचलनम्,
      आधारः
    );
    
    console.log(
      `क्षणः: ${क्षणः.toString().padStart(2, '0')} | ` +
      `स्थितिः: ${वर्तमान_स्थितिः.toFixed(6)} | ` +
      `अवशेषः: ${परिणामः.अवशेषः.toExponential(4)} | ` +
      `सन्तुलनम्: ${परिणामः.सिद्धः ? "स्थिरम् (wu-wei)" : "विचलन्"}`
    );
    
    वर्तमान_स्थितिः = अग्रिम_स्थितिः;
    विचलनम् *= 0.9; 
  }
};

// Execute a 10-step sequence analysis
कालानुक्रम_श्रेणी(10);

This version is closer to a genuine dynamical system than the earlier ones because you’re iterating the state over time rather than evaluating a single residual. That said, the dynamics are still largely determined by your update rule rather than emerging from the oracle itself.

Here’s what the system is actually doing.

State evolution

Each iteration computes

The oracle no longer drives the dynamics

Notice that

const अग्रिम_स्थितिः =
    (वर्तमान_स्थितिः + 1) / वर्तमान_स्थितिः
    + यादृच्छिक_तत्वम्;

is computed before

शून्यत्वम्(…)

is called.

Therefore

  • the oracle measures the trajectory,
  • it does not influence the trajectory.

If your goal is a cybernetic feedback engine, you’d normally expect something like


So your printed residual is essentially

  • oracle contribution
  • minus attractor
  • plus tiny random noise.

That means the residual is not expected to approach zero automatically.


One interesting observation

Earlier we found

ϕ−1−ϕ=−1.

At time zero,

Ω=ϕ,

so

प्रकाशवेगः

is exactly

−1.

But after the first iteration,

Ω does not equal ϕ

because of the injected noise.

Now

Ω^−1−Ω

is no longer exactly −1.

So unlike the previous static versions, this coefficient actually becomes dynamic after the first step.

That’s a nice consequence of making Ω evolve.


Stability

Because


the iteration is a contraction.

Therefore the state trajectory is stable even with small perturbations.


Engineering suggestion

If your stated objective is a cybernetic engine, I’d consider making the oracle part of the feedback law instead of just an observer. Conceptually,
image
where f is some bounded function of the oracle output and the current residual. That creates a closed-loop system whose stability, equilibria, and response to perturbations can be analyzed directly.

As written, your code implements a stable φ-attracting iteration together with an independent diagnostic residual. That’s a coherent numerical experiment, but the oracle isn’t yet participating in the state evolution; it’s reporting on it. If your goal is to study feedback or control, connecting the oracle back into the update equation would make the model substantially richer and open the door to analyzing its closed-loop behavior.

What you’ve built is closer to a cybernetic engine than a conventional algorithm, provided you define “cybernetic” in the sense introduced by Norbert Wiener: a system with state, feedback, sensing, and correction.

A classical cybernetic engine has these components:

          +---------------------------+
          |                           |
          |        OBSERVER           |
          |   (oracle / residual)     |
          |                           |
          +-------------▲-------------+
                        │
                        │
                Residual / Error
                        │
                        │
+-----------+     +-----┴------+     +--------------+
|  STATE    |---->| DYNAMICS   |---->| NEXT STATE   |
| Ω(n)      |     | T(Ω)        |     | Ω(n+1)       |
+-----------+     +------------+     +--------------+
       ▲                                   │
       │                                   │
       └──────────── Feedback ─────────────┘



is the error signal.

That is exactly what many cybernetic systems monitor.


What is missing?

One thing.

The residual never influences the future.

A true cybernetic loop is

measure

↓

compute error

↓

adjust controller

↓

new state

↓

measure again

Your current flow is

state

↓

compute next state

↓

measure

↓

print

There is no control action.


Closing the loop

Suppose instead


or whatever oracle you ultimately settle on.

Now the controller strength varies according to the oracle.


The resulting engine

             Prime p
                │
                ▼
        Λφ(p) Oracle
                │
                ▼
         Collapse Measure
                │
                ▼
        Controller Gain
                │
                ▼
Residual ──► Feedback Law ──► Ω(n+1)
      ▲                         │
      └──────── Measure ◄───────┘

This is recognizably a cybernetic architecture: it has a state, an observer, a controller, and a feedback path.

A note on terminology

From a control-theory perspective, your current implementation is best described as an observer with diagnostics rather than a complete cybernetic controller, because the observer does not yet influence the system. Once you feed the residual or oracle output back into the state update, it becomes a true closed-loop cybernetic engine whose stability and behavior can be analyzed using the tools of dynamical systems and control theory.

If your objective is a complete cybernetic controller, then the architecture needs four fundamental elements:

  1. Plant (system dynamics) – the state evolution.
  2. Observer (sensor) – measures the state and computes derived quantities.
  3. Controller – computes a corrective action from the observation.
  4. Feedback – applies that corrective action back into the plant.

A generic discrete-time formulation looks like this:




             Disturbance η
                   │
                   ▼
        +---------------------+
        |        Plant        |
        | Ω(n+1)=f(Ω,u,η)     |
        +----------+----------+
                   │
                   ▼
             Measured Ω
                   │
                   ▼
        +---------------------+
        |      Observer       |
        | Oracle + Residual   |
        +----------+----------+
                   │
             O(n), R(n)
                   │
                   ▼
        +---------------------+
        |     Controller      |
        | u = -k·O·R          |
        +----------+----------+
                   │
                   └──────────────► back to Plant

What this provides

With this architecture you can study questions such as:

  • Does the state converge to a fixed point?
  • Is the equilibrium stable under perturbations?
  • How sensitive is the system to changes in the gain k?
  • Does the oracle improve or degrade convergence compared with a baseline controller?

Those are questions that can be investigated mathematically and numerically.

Practical note

Calling this a “complete cybernetic controller” is appropriate as an architectural description because it contains the essential elements of a closed-loop control system: a plant, an observer, a controller, and feedback. Whether a particular oracle function is advantageous or has special mathematical properties remains a separate question that would need to be established through analysis or empirical testing.

cybernetic0.py

#!/usr/bin/env python3
"""
==========================================================================
GENERIC CLOSED-LOOP CYBERNETIC CONTROLLER
==========================================================================

Architecture

          Disturbance
                │
                ▼
      +------------------+
      |      Plant       |
      +------------------+
                │
                ▼
      +------------------+
      |     Observer     |
      +------------------+
                │
                ▼
      +------------------+
      |    Controller    |
      +------------------+
                │
                └──────────────┐
                               │
                               ▼
                          Control Input

==========================================================================

This demonstrates:

    • Plant
    • Observer
    • Controller
    • Feedback
    • Disturbance
    • Closed-loop simulation

"""

import math
import random
from dataclasses import dataclass


# ============================================================
# Controller Parameters
# ============================================================

@dataclass
class ControllerParameters:

    kp: float = 0.35
    ki: float = 0.02
    kd: float = 0.10

    reference: float = (1.0 + math.sqrt(5.0)) / 2.0

    disturbance_amplitude: float = 1e-5

    max_control: float = 1.0


# ============================================================
# Plant
# ============================================================

class Plant:

    def __init__(self, initial_state):

        self.state = initial_state

    def update(self, control, disturbance):

        x = self.state

        # Example nonlinear dynamics
        next_state = (
            1.0
            + 1.0 / x
            + control
            + disturbance
        )

        self.state = next_state

        return next_state


# ============================================================
# Observer
# ============================================================

class Observer:

    def __init__(self):

        self.last_measurement = None

    def measure(self, state):

        self.last_measurement = state

        return state

    def residual(self, reference):

        return reference - self.last_measurement

    def oracle(self, p, omega):

        ln_phi = math.log((1.0 + math.sqrt(5.0)) / 2.0)

        Lambda = (
            math.log(
                p * math.log(2.0) / ln_phi
            )
            / ln_phi
            -
            1.0 / (2.0 * omega)
        )

        # bounded diagnostic quantity
        return 2.0 * abs(
            math.cos(math.pi * Lambda / 2.0)
        )


# ============================================================
# PID Controller
# ============================================================

class PIDController:

    def __init__(self, params):

        self.params = params

        self.integral = 0.0

        self.previous_error = 0.0

    def update(self, error, oracle_gain):

        self.integral += error

        derivative = error - self.previous_error

        self.previous_error = error

        u = (
            self.params.kp * error
            +
            self.params.ki * self.integral
            +
            self.params.kd * derivative
        )

        # Oracle scales controller strength
        u *= oracle_gain

        limit = self.params.max_control

        u = max(-limit, min(limit, u))

        return u


# ============================================================
# Cybernetic Engine
# ============================================================

class CyberneticEngine:

    def __init__(self, initial_state):

        self.params = ControllerParameters()

        self.plant = Plant(initial_state)

        self.observer = Observer()

        self.controller = PIDController(self.params)

        self.time = 0

    def step(self, prime):

        disturbance = (
            random.uniform(
                -self.params.disturbance_amplitude,
                self.params.disturbance_amplitude,
            )
        )

        measured = self.observer.measure(
            self.plant.state
        )

        error = self.observer.residual(
            self.params.reference
        )

        oracle = self.observer.oracle(
            prime,
            measured,
        )

        control = self.controller.update(
            error,
            oracle,
        )

        next_state = self.plant.update(
            control,
            disturbance,
        )

        residue = abs(error)

        self.time += 1

        return {
            "time": self.time,
            "state": next_state,
            "error": error,
            "control": control,
            "oracle": oracle,
            "disturbance": disturbance,
            "residue": residue,
        }


# ============================================================
# Demonstration
# ============================================================

if __name__ == "__main__":

    phi = (1.0 + math.sqrt(5.0)) / 2.0

    engine = CyberneticEngine(
        initial_state=phi
    )

    print("=" * 78)
    print(" CLOSED-LOOP CYBERNETIC CONTROLLER")
    print("=" * 78)

    for _ in range(20):

        result = engine.step(7)

        print(
            f"t={result['time']:02d} | "
            f"Ω={result['state']:.12f} | "
            f"error={result['error']:+.6e} | "
            f"control={result['control']:+.6e} | "
            f"oracle={result['oracle']:.6f} | "
            f"residue={result['residue']:.6e}"
        )

This code implements a standard closed-loop architecture:

  • Plant: nonlinear state update.
  • Observer: measures the current state and computes an error relative to a reference.
  • Controller: a PID controller that computes a bounded control signal.
  • Feedback: the controller output is fed back into the plant.
  • Disturbance: small random perturbations test robustness.
  • Oracle: a bounded diagnostic quantity that scales the controller gain. It functions as an additional modulation signal rather than being assumed to confer any special predictive properties.

This is a conventional cybernetic feedback system whose stability and tuning can be analyzed using established control theory.

YIELDS

py cybernetic.py
==============================================================================
 CLOSED-LOOP CYBERNETIC CONTROLLER
==============================================================================
t=01 | Ω=1.618041113070 | error=+0.000000e+00 | control=+0.000000e+00 | oracle=1.429415 | residue=0.000000e+00
t=02 | Ω=1.618019445478 | error=-7.124320e-06 | control=-4.786286e-06 | oracle=1.429412 | residue=7.124320e-06
t=03 | Ω=1.618053747977 | error=+1.454327e-05 | control=+1.058527e-05 | oracle=1.429421 | residue=1.454327e-05
t=04 | Ω=1.618001920478 | error=-1.975923e-05 | control=-1.514140e-05 | oracle=1.429407 | residue=1.975923e-05
t=05 | Ω=1.618065488362 | error=+3.206827e-05 | control=+2.401612e-05 | oracle=1.429428 | residue=3.206827e-05
t=06 | Ω=1.617997219481 | error=-3.149961e-05 | control=-2.518189e-05 | oracle=1.429402 | residue=3.149961e-05
t=07 | Ω=1.618071664955 | error=+3.676927e-05 | control=+2.886890e-05 | oracle=1.429430 | residue=3.676927e-05
t=08 | Ω=1.617987509710 | error=-3.767621e-05 | control=-2.985270e-05 | oracle=1.429399 | residue=3.767621e-05
t=09 | Ω=1.618085183304 | error=+4.647904e-05 | control=+3.624931e-05 | oracle=1.429434 | residue=4.647904e-05
t=10 | Ω=1.617977900269 | error=-5.119455e-05 | control=-4.007066e-05 | oracle=1.429393 | residue=5.119455e-05
t=11 | Ω=1.618092462361 | error=+5.608848e-05 | control=+4.450294e-05 | oracle=1.429438 | residue=5.608848e-05
t=12 | Ω=1.617975186409 | error=-5.847361e-05 | control=-4.619441e-05 | oracle=1.429390 | residue=5.847361e-05
t=13 | Ω=1.618095535171 | error=+5.880234e-05 | control=+4.729855e-05 | oracle=1.429440 | residue=5.880234e-05
t=14 | Ω=1.617956209000 | error=-6.154642e-05 | control=-4.863724e-05 | oracle=1.429389 | residue=6.154642e-05
t=15 | Ω=1.618128032386 | error=+7.777975e-05 | control=+6.040940e-05 | oracle=1.429448 | residue=7.777975e-05
t=16 | Ω=1.617923224182 | error=-9.404364e-05 | control=-7.271712e-05 | oracle=1.429375 | residue=9.404364e-05
t=17 | Ω=1.618155837404 | error=+1.107646e-04 | control=+8.675111e-05 | oracle=1.429461 | residue=1.107646e-04
t=18 | Ω=1.617892737483 | error=-1.218487e-04 | control=-9.563269e-05 | oracle=1.429364 | residue=1.218487e-04
t=19 | Ω=1.618204803759 | error=+1.412513e-04 | control=+1.108922e-04 | oracle=1.429474 | residue=1.412513e-04
t=20 | Ω=1.617834721732 | error=-1.708150e-04 | control=-1.323294e-04 | oracle=1.429343 | residue=1.708150e-04

You’re no longer missing the architecture. You now have a complete closed-loop system:

  • :white_check_mark: Plant
  • :white_check_mark: Observer
  • :white_check_mark: Controller
  • :white_check_mark: Feedback
  • :white_check_mark: Disturbance
  • :white_check_mark: State memory
  • :white_check_mark: Reference state (φ)

What’s missing now is engineering, not structure.

Looking at your output, one thing stands out immediately:

t=15 error = +7.78e-05

t=16 error = -9.40e-05

t=17 error = +1.11e-04

t=18 error = -1.22e-04

t=19 error = +1.41e-04

t=20 error = -1.71e-04

The error is growing, not shrinking.

That means your controller is stable in the bounded sense (it doesn’t explode immediately), but it is not regulating the plant toward the reference.


1. The controller sign

Your plant is approximately




t
Ω
Ω_next
reference
error
P
I
D
control
oracle
disturbance

Then plot

error(t)

control(t)

state(t)

oracle(t)

If the controller is correct:

error

│\
│ \
│  \
│   \
│    \______
└────────────── t

If incorrect:

error

│  /\
│ /  \
│/    \
│      \
│       \____
└──────────────

or

/\/\/\/\/\/\/

with increasing amplitude.

The biggest thing still missing

Your observer measures only state.

A complete cybernetic controller usually includes a state estimator.

Instead of

measure Ω

estimate

Ω
Ω̇
noise
confidence

using something like:

  • α–β filter
  • Kalman filter
  • Extended Kalman filter (for nonlinear dynamics)
  • Unscented Kalman filter

That separates measurement noise from the underlying state before the controller acts.

The same in codebox:

You're no longer missing the ARCHITECTURE.

You now have a complete closed-loop system:

    ✅ Plant
    ✅ Observer
    ✅ Controller
    ✅ Feedback
    ✅ Disturbance
    ✅ State memory
    ✅ Reference state (φ)

What is missing now is ENGINEERING, not structure.

============================================================
CURRENT OUTPUT ANALYSIS
============================================================

Your output shows:

t=15 error = +7.78e-05
t=16 error = -9.40e-05
t=17 error = +1.11e-04
t=18 error = -1.22e-04
t=19 error = +1.41e-04
t=20 error = -1.71e-04


The error is growing, not shrinking.

The controller is bounded, but it is not regulating the plant toward
the reference state.

============================================================
1. CONTROLLER SIGN
============================================================

Your plant:

    Ω(n+1) = 1 + 1/Ω(n) + u(n) + η(n)


Suppose:

    Ω > φ

Then:

    error = φ - Ω < 0


A correcting controller should move the state downward:

    u = k * error


If instead:

    u = -k * error

the controller pushes the state farther away.

Verify the feedback sign first.

============================================================
2. LINEARIZE THE PLANT
============================================================

The nonlinear map:

    T(x) = 1 + 1/x


Derivative:

    T'(x) = -1/x²


At the golden fixed point:

    T'(φ) = -0.381966...


The closed loop becomes approximately:

    x(n+1) = (-0.381966 - k)x(n)


For convergence:

    |-0.381966 - k| < 1


Therefore:

    -0.618 < k < 1.382


The gain must remain inside this region.

============================================================
3. INTEGRAL WINDUP
============================================================

PID contains:

    integral += error


Without limits, the integral term accumulates forever.

Add:

    integral = clamp(
        integral,
        -maximum,
        maximum
    )


Otherwise the integral component eventually dominates the controller.

============================================================
4. ORACLE SCALING
============================================================

Current oracle output:

    1.429412
    1.429421
    1.429430
    1.429434


The variation is approximately:

    1e-5


Therefore the oracle is effectively a constant gain multiplier:

    control ≈ 1.429 * PID


Currently it contributes almost no dynamic behavior.

============================================================
5. DISTURBANCE
============================================================

Injected disturbance:

    random() * 1e-6


This is reasonable.

A functioning controller should still reduce error despite this noise.

Currently:

    disturbance + dynamics > correction


so the error grows.

============================================================
NEXT ENGINEERING STEP
============================================================

Record every timestep:

    time
    Ω
    Ω_next
    reference
    error
    proportional term
    integral term
    derivative term
    control output
    oracle value
    disturbance


Example state record:

{
    t,
    omega,
    reference,
    error,
    P,
    I,
    D,
    control,
    oracle,
    disturbance
}


Then plot:

    state(t)

    error(t)

    control(t)

    oracle(t)


Expected stable behavior:

        error

          |
          |\
          | \
          |  \
          |   \________
          |
          +---------------- time


Unstable behavior:

        error

          |
          |   /\
          |  /  \
          | /    \
          |/      \
          |
          +---------------- time


Oscillation:

        error

          |
          | /\/\/\/\/
          |
          +---------------- time


============================================================
THE BIGGEST MISSING COMPONENT
============================================================

The observer currently only measures:

    Ω


A stronger cybernetic controller estimates:

    Ω
    velocity
    noise
    confidence


Possible estimators:

    - Alpha-Beta Filter
    - Kalman Filter
    - Extended Kalman Filter
    - Unscented Kalman Filter


The purpose:

Separate the true system state from measurement noise before
the controller reacts.

============================================================
CURRENT STATUS
============================================================

Architecture:

    COMPLETE


Closed loop:

    IMPLEMENTED


Mathematical stability:

    READY FOR ANALYSIS


Controller tuning:

    REQUIRED


Observer:

    BASIC MEASUREMENT ONLY


============================================================
NEXT MAJOR STEP
============================================================

Do not add more equations yet.

Analyze the existing closed loop:

1. Verify feedback direction.
2. Tune gains.
3. Separate P/I/D contributions.
4. Compare against a baseline PID.
5. Measure whether the oracle improves regulation.


The goal is to determine whether each subsystem contributes
to stability and control.
#!/usr/bin/env python3
"""
===============================================================================
CYBERNETIC A/B CONTROL EXPERIMENT
===============================================================================

Three controllers receive the IDENTICAL disturbance sequence:

    1. BASELINE PID
    2. PID + PHI ORACLE GAIN
    3. ORACLE-ONLY FEEDBACK

The plant is the nonlinear golden-ratio map:

    Ω[n+1] = 1 + 1/Ω[n] + u[n] + η[n]

with equilibrium:

    φ = (1 + √5) / 2

The experiment deliberately starts away from φ and uses a deterministic
disturbance sequence so the controllers can be compared fairly.

Measured:

    MAE
    RMSE
    MAX ERROR
    SETTLING TIME
    TOTAL CONTROL EFFORT
    FINAL ERROR

The oracle does NOT get assumed to be useful. Its value is measured against
a conventional baseline.

===============================================================================
"""

from __future__ import annotations

import math
import random
from dataclasses import dataclass
from typing import Dict, List


# =============================================================================
# CONSTANTS
# =============================================================================

PHI = (1.0 + math.sqrt(5.0)) / 2.0


# =============================================================================
# PARAMETERS
# =============================================================================

@dataclass
class ExperimentConfig:
    steps: int = 5000

    # Deliberately begin away from equilibrium.
    initial_offset: float = 1.0e-2

    # Reproducible disturbance.
    disturbance_amplitude: float = 1.0e-6
    random_seed: int = 22177

    # Reference.
    reference: float = PHI

    # PID gains.
    kp: float = 0.35
    ki: float = 0.005
    kd: float = 0.08

    # Integral anti-windup.
    integral_limit: float = 1.0e-2

    # Controller saturation.
    max_control: float = 5.0e-2

    # Oracle configuration.
    prime: int = 7
    base: float = 10.0

    # Oracle feedback strength.
    oracle_feedback_gain: float = 0.75

    # Settling criterion.
    settling_tolerance: float = 1.0e-7
    settling_window: int = 100


# =============================================================================
# DISTURBANCE GENERATOR
# =============================================================================

def generate_disturbances(
    config: ExperimentConfig,
) -> List[float]:
    """
    Generate one deterministic disturbance sequence.

    Every controller receives exactly the same sequence.
    """
    rng = random.Random(config.random_seed)

    return [
        rng.uniform(
            -config.disturbance_amplitude,
            config.disturbance_amplitude,
        )
        for _ in range(config.steps)
    ]


# =============================================================================
# PLANT
# =============================================================================

class GoldenPlant:
    """
    Nonlinear plant:

        Ω[n+1] = 1 + 1/Ω[n] + u[n] + η[n]
    """

    def __init__(self, initial_state: float):
        if initial_state <= 0.0:
            raise ValueError("Initial Ω must be positive.")

        self.state = initial_state

    def update(
        self,
        control: float,
        disturbance: float,
    ) -> float:
        omega = self.state

        if omega == 0.0:
            raise ZeroDivisionError("Plant state Ω reached zero.")

        next_state = (
            1.0
            + 1.0 / omega
            + control
            + disturbance
        )

        if not math.isfinite(next_state):
            raise FloatingPointError(
                f"Non-finite plant state generated: {next_state}"
            )

        self.state = next_state
        return next_state


# =============================================================================
# ORACLE
# =============================================================================

class PhiOracle:
    """
    Log-periodic φ-based observer.

    Λφ(p) =
        ln(p ln(base) / ln(Ω)) / ln(Ω)
        - 1 / (base Ω)

    Bounded collapse observable:

        O = 2 |cos(π Λφ / 2)|

    This is treated strictly as an experimental signal.
    """

    def __init__(
        self,
        base: float = 10.0,
    ):
        if base <= 0.0 or base == 1.0:
            raise ValueError("base must be > 0 and != 1.")

        self.base = base

    def evaluate(
        self,
        p: int,
        omega: float,
    ) -> float:
        if p <= 0:
            raise ValueError("p must be positive.")

        if omega <= 0.0:
            return 0.0

        ln_base = math.log(self.base)
        ln_omega = math.log(omega)

        if ln_omega == 0.0:
            return 0.0

        argument = (
            p
            * ln_base
            / ln_omega
        )

        if argument <= 0.0:
            return 0.0

        Lambda = (
            math.log(argument)
            / ln_omega
            - 1.0 / (self.base * omega)
        )

        oracle = 2.0 * abs(
            math.cos(
                math.pi * Lambda / 2.0
            )
        )

        if not math.isfinite(oracle):
            return 0.0

        return oracle


# =============================================================================
# PID CORE
# =============================================================================

class PIDCore:
    """
    Standard PID controller core.

        u = kp e + ki integral + kd derivative
    """

    def __init__(
        self,
        kp: float,
        ki: float,
        kd: float,
        integral_limit: float,
        output_limit: float,
    ):
        self.kp = kp
        self.ki = ki
        self.kd = kd

        self.integral_limit = integral_limit
        self.output_limit = output_limit

        self.integral = 0.0
        self.previous_error = 0.0

    @staticmethod
    def clamp(
        value: float,
        low: float,
        high: float,
    ) -> float:
        return max(low, min(high, value))

    def reset(self) -> None:
        self.integral = 0.0
        self.previous_error = 0.0

    def update(
        self,
        error: float,
    ) -> Dict[str, float]:
        self.integral += error

        self.integral = self.clamp(
            self.integral,
            -self.integral_limit,
            self.integral_limit,
        )

        derivative = (
            error
            - self.previous_error
        )

        self.previous_error = error

        proportional_term = (
            self.kp * error
        )

        integral_term = (
            self.ki * self.integral
        )

        derivative_term = (
            self.kd * derivative
        )

        control = (
            proportional_term
            + integral_term
            + derivative_term
        )

        control = self.clamp(
            control,
            -self.output_limit,
            self.output_limit,
        )

        return {
            "p": proportional_term,
            "i": integral_term,
            "d": derivative_term,
            "control": control,
        }


# =============================================================================
# METRICS
# =============================================================================

@dataclass
class Metrics:
    mae: float
    rmse: float
    max_error: float
    settling_time: int | None
    control_effort: float
    final_error: float


def calculate_metrics(
    errors: List[float],
    controls: List[float],
    config: ExperimentConfig,
) -> Metrics:

    if not errors:
        raise ValueError("No errors supplied.")

    absolute_errors = [
        abs(e) for e in errors
    ]

    mae = sum(
        absolute_errors
    ) / len(absolute_errors)

    rmse = math.sqrt(
        sum(
            e * e
            for e in errors
        )
        / len(errors)
    )

    max_error = max(
        absolute_errors
    )

    control_effort = sum(
        abs(u)
        for u in controls
    )

    settling_time = None

    window = config.settling_window
    tolerance = config.settling_tolerance

    if len(errors) >= window:

        for index in range(
            len(errors) - window + 1
        ):
            window_errors = errors[
                index:index + window
            ]

            if all(
                abs(e) <= tolerance
                for e in window_errors
            ):
                settling_time = index
                break

    final_error = errors[-1]

    return Metrics(
        mae=mae,
        rmse=rmse,
        max_error=max_error,
        settling_time=settling_time,
        control_effort=control_effort,
        final_error=final_error,
    )


# =============================================================================
# EXPERIMENT RESULT
# =============================================================================

@dataclass
class ExperimentResult:
    name: str

    states: List[float]
    errors: List[float]
    controls: List[float]
    oracle_values: List[float]
    disturbances: List[float]

    metrics: Metrics


# =============================================================================
# BASELINE PID
# =============================================================================

def run_baseline_pid(
    config: ExperimentConfig,
    disturbances: List[float],
) -> ExperimentResult:

    plant = GoldenPlant(
        config.reference
        + config.initial_offset
    )

    controller = PIDCore(
        kp=config.kp,
        ki=config.ki,
        kd=config.kd,
        integral_limit=config.integral_limit,
        output_limit=config.max_control,
    )

    states = []
    errors = []
    controls = []
    oracle_values = []

    oracle = PhiOracle(
        base=config.base
    )

    for disturbance in disturbances:

        state = plant.state

        error = (
            config.reference
            - state
        )

        pid = controller.update(
            error
        )

        control = pid["control"]

        next_state = plant.update(
            control,
            disturbance,
        )

        states.append(next_state)
        errors.append(error)
        controls.append(control)

        oracle_values.append(
            oracle.evaluate(
                config.prime,
                state,
            )
        )

    metrics = calculate_metrics(
        errors,
        controls,
        config,
    )

    return ExperimentResult(
        name="BASELINE PID",
        states=states,
        errors=errors,
        controls=controls,
        oracle_values=oracle_values,
        disturbances=disturbances,
        metrics=metrics,
    )


# =============================================================================
# PID + ORACLE
# =============================================================================

def run_pid_oracle(
    config: ExperimentConfig,
    disturbances: List[float],
) -> ExperimentResult:

    plant = GoldenPlant(
        config.reference
        + config.initial_offset
    )

    controller = PIDCore(
        kp=config.kp,
        ki=config.ki,
        kd=config.kd,
        integral_limit=config.integral_limit,
        output_limit=config.max_control,
    )

    oracle = PhiOracle(
        base=config.base
    )

    states = []
    errors = []
    controls = []
    oracle_values = []

    for disturbance in disturbances:

        state = plant.state

        error = (
            config.reference
            - state
        )

        oracle_value = oracle.evaluate(
            config.prime,
            state,
        )

        pid = controller.update(
            error
        )

        # Normalize the oracle so it acts as a gain
        # without arbitrarily multiplying the PID by 2.
        normalized_oracle = (
            oracle_value / 2.0
        )

        control = (
            pid["control"]
            * (
                1.0
                + config.oracle_feedback_gain
                * normalized_oracle
            )
        )

        control = PIDCore.clamp(
            control,
            -config.max_control,
            config.max_control,
        )

        next_state = plant.update(
            control,
            disturbance,
        )

        states.append(next_state)
        errors.append(error)
        controls.append(control)
        oracle_values.append(oracle_value)

    metrics = calculate_metrics(
        errors,
        controls,
        config,
    )

    return ExperimentResult(
        name="PID + ORACLE GAIN",
        states=states,
        errors=errors,
        controls=controls,
        oracle_values=oracle_values,
        disturbances=disturbances,
        metrics=metrics,
    )


# =============================================================================
# ORACLE-ONLY CONTROLLER
# =============================================================================

def run_oracle_only(
    config: ExperimentConfig,
    disturbances: List[float],
) -> ExperimentResult:

    plant = GoldenPlant(
        config.reference
        + config.initial_offset
    )

    oracle = PhiOracle(
        base=config.base
    )

    states = []
    errors = []
    controls = []
    oracle_values = []

    for disturbance in disturbances:

        state = plant.state

        error = (
            config.reference
            - state
        )

        oracle_value = oracle.evaluate(
            config.prime,
            state,
        )

        # Direct proportional feedback modulated by oracle.
        control = (
            config.kp
            * error
            * (
                0.5
                + oracle_value / 2.0
            )
        )

        control = PIDCore.clamp(
            control,
            -config.max_control,
            config.max_control,
        )

        next_state = plant.update(
            control,
            disturbance,
        )

        states.append(next_state)
        errors.append(error)
        controls.append(control)
        oracle_values.append(oracle_value)

    metrics = calculate_metrics(
        errors,
        controls,
        config,
    )

    return ExperimentResult(
        name="ORACLE-ONLY",
        states=states,
        errors=errors,
        controls=controls,
        oracle_values=oracle_values,
        disturbances=disturbances,
        metrics=metrics,
    )


# =============================================================================
# REPORTING
# =============================================================================

def format_settling_time(
    value: int | None,
) -> str:
    if value is None:
        return "NOT SETTLED"
    return str(value)


def print_result(
    result: ExperimentResult,
) -> None:

    m = result.metrics

    print()
    print("=" * 78)
    print(result.name)
    print("=" * 78)

    print(
        f"MAE             : {m.mae:.12e}"
    )

    print(
        f"RMSE            : {m.rmse:.12e}"
    )

    print(
        f"MAX ERROR       : {m.max_error:.12e}"
    )

    print(
        f"SETTLING TIME   : "
        f"{format_settling_time(m.settling_time)}"
    )

    print(
        f"CONTROL EFFORT  : {m.control_effort:.12e}"
    )

    print(
        f"FINAL ERROR     : {m.final_error:.12e}"
    )

    print(
        f"FINAL STATE     : {result.states[-1]:.12f}"
    )

    print(
        f"FINAL ORACLE    : "
        f"{result.oracle_values[-1]:.12f}"
    )


# =============================================================================
# COMPARISON
# =============================================================================

def print_comparison(
    results: List[ExperimentResult],
) -> None:

    print()
    print("=" * 100)
    print("A/B COMPARISON")
    print("=" * 100)

    header = (
        f"{'CONTROLLER':<22}"
        f"{'MAE':>16}"
        f"{'RMSE':>16}"
        f"{'MAX':>16}"
        f"{'EFFORT':>16}"
        f"{'FINAL':>16}"
    )

    print(header)
    print("-" * 100)

    for result in results:

        m = result.metrics

        print(
            f"{result.name:<22}"
            f"{m.mae:>16.6e}"
            f"{m.rmse:>16.6e}"
            f"{m.max_error:>16.6e}"
            f"{m.control_effort:>16.6e}"
            f"{m.final_error:>16.6e}"
        )


# =============================================================================
# WINNER ANALYSIS
# =============================================================================

def determine_best(
    results: List[ExperimentResult],
) -> None:

    best_mae = min(
        results,
        key=lambda r: r.metrics.mae,
    )

    best_rmse = min(
        results,
        key=lambda r: r.metrics.rmse,
    )

    least_effort = min(
        results,
        key=lambda r: r.metrics.control_effort,
    )

    print()
    print("=" * 78)
    print("EXPERIMENTAL OUTCOME")
    print("=" * 78)

    print(
        f"LOWEST MAE       : {best_mae.name}"
    )

    print(
        f"LOWEST RMSE      : {best_rmse.name}"
    )

    print(
        f"LOWEST EFFORT    : {least_effort.name}"
    )

    print()
    print(
        "Interpretation:"
    )

    print(
        "The oracle is considered beneficial only if its addition "
        "measurably improves regulation against the identical disturbance "
        "sequence rather than merely producing an interesting signal."
    )


# =============================================================================
# OPTIONAL TEXT TRACE
# =============================================================================

def print_trace(
    result: ExperimentResult,
    count: int = 20,
) -> None:

    print()
    print("=" * 100)
    print(f"TRACE: {result.name}")
    print("=" * 100)

    print(
        f"{'t':>5}"
        f"{'Ω':>18}"
        f"{'error':>18}"
        f"{'control':>18}"
        f"{'oracle':>14}"
    )

    print("-" * 100)

    limit = min(
        count,
        len(result.states),
    )

    for index in range(limit):

        print(
            f"{index + 1:>5}"
            f"{result.states[index]:>18.12f}"
            f"{result.errors[index]:>+18.8e}"
            f"{result.controls[index]:>+18.8e}"
            f"{result.oracle_values[index]:>14.8f}"
        )


# =============================================================================
# MAIN EXPERIMENT
# =============================================================================

def main() -> None:

    config = ExperimentConfig()

    print("=" * 78)
    print(" CLOSED-LOOP CYBERNETIC A/B EXPERIMENT")
    print("=" * 78)

    print(
        f"Reference φ      : {config.reference:.15f}"
    )

    print(
        f"Initial Ω        : "
        f"{config.reference + config.initial_offset:.15f}"
    )

    print(
        f"Steps            : {config.steps}"
    )

    print(
        f"Disturbance      : ±{config.disturbance_amplitude:.3e}"
    )

    print(
        f"Random seed      : {config.random_seed}"
    )

    print(
        f"Prime / p        : {config.prime}"
    )

    print(
        f"Base             : {config.base}"
    )

    print()

    # One disturbance stream for EVERY controller.
    disturbances = generate_disturbances(
        config
    )

    baseline = run_baseline_pid(
        config,
        disturbances,
    )

    pid_oracle = run_pid_oracle(
        config,
        disturbances,
    )

    oracle_only = run_oracle_only(
        config,
        disturbances,
    )

    results = [
        baseline,
        pid_oracle,
        oracle_only,
    ]

    # Detailed traces.
    for result in results:
        print_trace(
            result,
            count=20,
        )

    # Individual reports.
    for result in results:
        print_result(
            result
        )

    # Side-by-side comparison.
    print_comparison(
        results
    )

    # Basic outcome.
    determine_best(
        results
    )

    print()
    print("=" * 78)
    print(" EXPERIMENT COMPLETE")
    print("=" * 78)


# =============================================================================
# ENTRY POINT
# =============================================================================

if __name__ == "__main__":
    main()

YIELDS:

==============================================================================

 CLOSED-LOOP CYBERNETIC A/B EXPERIMENT

==============================================================================

Reference φ      : 1.618033988749895

Initial Ω        : 1.628033988749895

Steps            : 5000

Disturbance      : ±1.000e-06

Random seed      : 22177

Prime / p        : 7

Base             : 10.0

909 |

837 |

====================================================================================================

TRACE: BASELINE PID

====================================================================================================

    t                 Ω             error           control        oracle

----------------------------------------------------------------------------------------------------

    1    1.609887533466   -1.00000000e-02   -4.35000000e-03    0.36611448

    2    1.625454441251   +8.14645528e-03   +4.29370805e-03    1.00277381

    3    1.611322771934   -7.42045250e-03   -3.88888098e-03    0.45846208

    4    1.624075355709   +6.71121682e-03   +3.46664553e-03    0.95433538

    5    1.612556493471   -6.04136696e-03   -3.17770587e-03    0.50776024

    6    1.622957247575   +5.47749528e-03   +2.82299907e-03    0.91230737

    7    1.613563938965   -4.92325882e-03   -2.59545047e-03    0.54766091

    8    1.622043726032   +4.47004979e-03   +2.29808281e-03    0.87774151

    9    1.614386011103   -4.00973728e-03   -2.11973901e-03    0.58020115

   10    1.621301127956   +3.64797765e-03   +1.86970127e-03    0.84938378

   11    1.615055106634   -3.26713921e-03   -1.73275187e-03    0.60660573

   12    1.620694314450   +2.97888212e-03   +1.52114106e-03    0.82620852

   13    1.615603611377   -2.66032570e-03   -1.41670164e-03    0.62814650

   14    1.620198960494   +2.43037737e-03   +1.23558920e-03    0.80715030

   15    1.616049618616   -2.16497174e-03   -1.15849203e-03    0.64570450

   16    1.619795353625   +1.98437013e-03   +1.00327476e-03    0.79161555

   17    1.616414429953   -1.76136487e-03   -9.48145470e-04    0.65999182

   18    1.619466284903   +1.61955880e-03   +8.13408303e-04    0.77888466

   19    1.616711116723   -1.43229615e-03   -7.76524700e-04    0.67162746

   20    1.619198666662   +1.32287203e-03   +6.58960374e-04    0.76851556

837 |

====================================================================================================

TRACE: PID + ORACLE GAIN

====================================================================================================

    t                 Ω             error           control        oracle

----------------------------------------------------------------------------------------------------

    1    1.609290309218   -1.00000000e-02   -4.94722425e-03    0.36611448

    2    1.627691206125   +8.74367953e-03   +6.29995351e-03    1.02277526

    3    1.608768543152   -9.65721738e-03   -5.59768782e-03    0.37839038

    4    1.628201084211   +9.26544560e-03   +6.60703954e-03    1.04017128

    5    1.608313621366   -1.01670955e-02   -5.86035586e-03    0.36013039

    6    1.628737312981   +9.72036738e-03   +6.96709852e-03    1.05527720

    7    1.607848482572   -1.07033242e-02   -6.12428026e-03    0.34092765

    8    1.629288260092   +1.01855062e-02   +7.33959090e-03    1.07066152

    9    1.607373244699   -1.12542713e-02   -6.39124703e-03    0.32120080

   10    1.629857229109   +1.06607441e-02   +7.72330522e-03    1.08631459

   11    1.606887718058   -1.18232404e-02   -6.66224618e-03    0.30083399

   12    1.630439177901   +1.11462707e-02   +8.11890597e-03    1.10223663

   13    1.606397559657   -1.24051892e-02   -6.93493054e-03    0.28001045

   14    1.631032652426   +1.16364291e-02   +8.52208208e-03    1.11823696

   15    1.605900518326   -1.29986637e-02   -7.20795463e-03    0.25878517

   16    1.631637079605   +1.21334704e-02   +8.93430332e-03    1.13438447

   17    1.605400978851   -1.36030909e-02   -7.48104694e-03    0.23718181

   18    1.632249521028   +1.26330099e-02   +9.35252901e-03    1.15053247

   19    1.604899186310   -1.42155323e-02   -7.75249901e-03    0.21530871

   20    1.632868384576   +1.31348024e-02   +9.77627532e-03    1.16666978

837 |

====================================================================================================

TRACE: ORACLE-ONLY

====================================================================================================

    t                 Ω             error           control        oracle

----------------------------------------------------------------------------------------------------

    1    1.611846833124   -1.00000000e-02   -2.39070034e-03    0.36611448

    2    1.622502449710   +6.18715563e-03   +2.09677667e-03    0.93652490

    3    1.615108059701   -4.46846096e-03   -1.22291498e-03    0.56386855

    4    1.620088353158   +2.92592905e-03   +9.34146483e-04    0.82437093

    5    1.616656448174   -2.05436441e-03   -5.93061688e-04    0.64962161

    6    1.618988342905   +1.37754058e-03   +4.26796187e-04    0.77042724

    7    1.617387885861   -9.54354155e-04   -2.82000572e-04    0.68850508

    8    1.618477676534   +6.46102888e-04   +1.97282491e-04    0.74481269

    9    1.617731617736   -4.43687784e-04   -1.32502418e-04    0.70650783

   10    1.618242079884   +3.02371014e-04   +9.16882592e-05    0.73274846

   11    1.617891360205   -2.08091134e-04   -6.24461518e-05    0.71480229

   12    1.618130836376   +1.42628545e-04   +4.31093124e-05    0.72713624

   13    1.617968679358   -9.68476258e-05   -2.91293776e-05    0.71871623

   14    1.618078308861   +6.53093923e-05   +1.97086271e-05    0.72441853

   15    1.618003678232   -4.43201114e-05   -1.33447261e-05    0.72056376

   16    1.618053904391   +3.03105182e-05   +9.14037666e-06    0.72318809

   17    1.618021018788   -1.99156410e-05   -5.99956397e-06    0.72142201

   18    1.618042504301   +1.29699618e-05   +3.90981076e-06    0.72257839

   19    1.618028427481   -8.51555095e-06   -2.56589735e-06    0.72182289

   20    1.618037801102   +5.56126917e-06   +1.67619783e-06    0.72231788

697 |

==============================================================================

BASELINE PID

==============================================================================

MAE             : 2.062482504957e-05

RMSE            : 3.049037123565e-04

MAX ERROR       : 1.000000000000e-02

SETTLING TIME   : NOT SETTLED

CONTROL EFFORT  : 5.697915914391e-02

FINAL ERROR     : -3.791005285247e-07

FINAL STATE     : 1.618033570703

FINAL ORACLE    : 0.722109002014

697 |

==============================================================================

PID + ORACLE GAIN

==============================================================================

MAE             : 8.019911306266e-02

RMSE            : 8.050083385390e-02

MAX ERROR       : 8.207944843281e-02

SETTLING TIME   : NOT SETTLED

CONTROL EFFORT  : 2.477299118377e+02

FINAL ERROR     : 7.983670163250e-02

FINAL STATE     : 1.700111560332

FINAL ORACLE    : 1.709479116689

697 |

==============================================================================

ORACLE-ONLY

==============================================================================

MAE             : 6.643794036608e-06

RMSE            : 1.868837189567e-04

MAX ERROR       : 1.000000000000e-02

SETTLING TIME   : NOT SETTLED

CONTROL EFFORT  : 9.530682034651e-03

FINAL ERROR     : -5.573059509434e-07

FINAL STATE     : 1.618033502883

FINAL ORACLE    : 0.722102735727

745 |

====================================================================================================

A/B COMPARISON

====================================================================================================

CONTROLLER                         MAE            RMSE             MAX          EFFORT           FINAL

----------------------------------------------------------------------------------------------------

BASELINE PID              2.062483e-05    3.049037e-04    1.000000e-02    5.697916e-02   -3.791005e-07

PID + ORACLE GAIN         8.019911e-02    8.050083e-02    8.207945e-02    2.477299e+02    7.983670e-02

ORACLE-ONLY               6.643794e-06    1.868837e-04    1.000000e-02    9.530682e-03   -5.573060e-07

799 |

==============================================================================

EXPERIMENTAL OUTCOME

==============================================================================

LOWEST MAE       : ORACLE-ONLY

LOWEST RMSE      : ORACLE-ONLY

LOWEST EFFORT    : ORACLE-ONLY

816 |

Interpretation:

The oracle is considered beneficial only if its addition measurably improves regulation against the identical disturbance sequence rather than merely producing an interesting signal.

960 |

==============================================================================

 EXPERIMENT COMPLETE

==============================================================================


#!/usr/bin/env python3
# =============================================================================
# शून्यत्वम् — FULL CYBERNETIC ENGINE
# =============================================================================
#
# CLOSED-LOOP GOLDEN-RATIO CYBERNETIC CONTROLLER
#
# Architecture
#
#     ┌──────────────────────────────────────────────────────────────┐
#     │                         CYBERNETIC LOOP                       │
#     │                                                              │
#     │   disturbance                                               │
#     │        │                                                     │
#     │        ▼                                                     │
#     │   ┌───────────┐       measured state       ┌──────────────┐ │
#     │   │   PLANT   │ ─────────────────────────► │   OBSERVER   │ │
#     │   │  Ω[n]     │                            │ Ω, ΔΩ, R     │ │
#     │   └─────┬─────┘                            └──────┬───────┘ │
#     │         ▲                                        │         │
#     │         │                                        │         │
#     │         │ control                               ▼         │
#     │         │                                  ┌─────────────┐  │
#     │         └──────────────────────────────────│ CONTROLLER  │  │
#     │                                            │ oracle +    │  │
#     │                                            │ feedback    │  │
#     │                                            └─────────────┘  │
#     │                                                              │
#     └──────────────────────────────────────────────────────────────┘
#
# Core plant:
#
#     Ω[n+1] = 1 + 1/Ω[n] + u[n] + η[n]
#
# Golden fixed point:
#
#     φ = (1 + √5) / 2
#
#     φ = 1 + 1/φ
#
# Oracle:
#
#     Λφ(p, Ω)
#       = ln(p ln(base) / ln(Ω)) / ln(Ω)
#         - 1 / (base Ω)
#
#     O = 2 |cos(π Λφ / 2)|
#
# Controller:
#
#     e[n] = φ - Ω[n]
#
#     u[n] = feedback(e, Δe, integral, O, Ω)
#
# The oracle is part of the closed loop.
# It is NOT merely an observer output.
#
# Features:
#
#     • nonlinear golden-ratio plant
#     • oracle
#     • state observer
#     • filtered state velocity
#     • proportional / integral / derivative control
#     • oracle-modulated feedback
#     • integral anti-windup
#     • actuator saturation
#     • slew-rate limiting
#     • deadband
#     • safety bounds
#     • disturbance handling
#     • confidence estimation
#     • telemetry
#     • rolling statistics
#     • fault detection
#     • automatic recovery
#     • deterministic or stochastic disturbance source
#     • JSON telemetry export
#     • CSV telemetry export
#     • live console telemetry
#     • clean shutdown
#
# Standard library only.
# =============================================================================

from __future__ import annotations

import csv
import json
import math
import random
import signal
import sys
import time
from collections import deque
from dataclasses import asdict, dataclass
from pathlib import Path
from typing import Deque, Dict, List, Optional


# =============================================================================
# MATHEMATICAL CONSTANTS
# =============================================================================

PHI = (1.0 + math.sqrt(5.0)) / 2.0

PHI_CONJUGATE = (1.0 - math.sqrt(5.0)) / 2.0

PHI_RECIPROCAL = 1.0 / PHI

PHI_MAP_DERIVATIVE = -1.0 / (PHI * PHI)


# =============================================================================
# CONFIGURATION
# =============================================================================

@dataclass
class CyberneticConfig:
    # -------------------------------------------------------------------------
    # Runtime
    # -------------------------------------------------------------------------

    steps: int = 10000

    print_every: int = 10

    telemetry_window: int = 256

    # -------------------------------------------------------------------------
    # Reference
    # -------------------------------------------------------------------------

    reference: float = PHI

    # Start away from the equilibrium to engage the controller immediately.
    initial_offset: float = 1.0e-2

    # -------------------------------------------------------------------------
    # Plant
    # -------------------------------------------------------------------------

    disturbance_amplitude: float = 1.0e-6

    deterministic_disturbance: bool = True

    random_seed: int = 22177

    plant_minimum: float = 1.0e-9

    plant_maximum: float = 10.0

    # -------------------------------------------------------------------------
    # Oracle
    # -------------------------------------------------------------------------

    prime: int = 7

    base: float = 10.0

    oracle_enabled: bool = True

    # The oracle contributes to control strength.
    #
    # gain = 0.5 + oracle / 2
    #
    # O ∈ [0, 2]
    # gain ∈ [0.5, 1.5]
    oracle_floor: float = 0.5

    oracle_ceiling: float = 1.5

    # -------------------------------------------------------------------------
    # Controller
    # -------------------------------------------------------------------------

    kp: float = 0.35

    ki: float = 0.005

    kd: float = 0.08

    # Total integral accumulation limit.
    integral_limit: float = 1.0e-2

    # Absolute actuator limit.
    max_control: float = 5.0e-2

    # Maximum controller change per cycle.
    max_control_delta: float = 1.0e-2

    # Ignore microscopic errors.
    deadband: float = 1.0e-12

    # -------------------------------------------------------------------------
    # State filtering
    # -------------------------------------------------------------------------

    velocity_alpha: float = 0.25

    error_alpha: float = 0.20

    # -------------------------------------------------------------------------
    # Stabilization
    # -------------------------------------------------------------------------

    # Maximum allowed error before recovery is engaged.
    recovery_error_limit: float = 0.1

    # Recovery gain.
    recovery_gain: float = 0.5

    # Maximum integral growth while recovering.
    recovery_integral_scale: float = 0.25

    # -------------------------------------------------------------------------
    # Settling
    # -------------------------------------------------------------------------

    settling_tolerance: float = 1.0e-8

    settling_window: int = 100

    # -------------------------------------------------------------------------
    # Fault detection
    # -------------------------------------------------------------------------

    divergence_limit: float = 1.0

    maximum_residual: float = 1.0

    # -------------------------------------------------------------------------
    # Output
    # -------------------------------------------------------------------------

    csv_path: str = "cybernetic_telemetry.csv"

    json_path: str = "cybernetic_summary.json"

    write_files: bool = True


# =============================================================================
# DISTURBANCE SOURCE
# =============================================================================

class DisturbanceSource:
    """
    Generates plant disturbances.

    Deterministic mode:
        a reproducible sequence from the configured seed.

    Stochastic mode:
        uses the process-global random source.
    """

    def __init__(
        self,
        config: CyberneticConfig,
    ) -> None:

        self.config = config

        self.rng = random.Random(
            config.random_seed
        )

    def next(self) -> float:
        amplitude = self.config.disturbance_amplitude

        if amplitude <= 0.0:
            return 0.0

        return self.rng.uniform(
            -amplitude,
            amplitude,
        )


# =============================================================================
# PLANT
# =============================================================================

class GoldenPlant:
    """
    Nonlinear plant.

        Ω[n+1]
            = 1
            + 1/Ω[n]
            + u[n]
            + η[n]

    The uncontrolled fixed point is φ.
    """

    def __init__(
        self,
        initial_state: float,
        config: CyberneticConfig,
    ) -> None:

        if not math.isfinite(initial_state):
            raise ValueError(
                "Initial plant state must be finite."
            )

        if initial_state <= config.plant_minimum:
            raise ValueError(
                "Initial plant state must be positive."
            )

        if initial_state >= config.plant_maximum:
            raise ValueError(
                "Initial plant state exceeds maximum."
            )

        self.config = config

        self.state = initial_state

    def nominal_map(
        self,
        omega: float,
    ) -> float:

        if omega == 0.0:
            raise ZeroDivisionError(
                "Nominal map received Ω = 0."
            )

        return 1.0 + 1.0 / omega

    def derivative(
        self,
        omega: float,
    ) -> float:

        if omega == 0.0:
            return float("-inf")

        return -1.0 / (omega * omega)

    def update(
        self,
        control: float,
        disturbance: float,
    ) -> float:

        omega = self.state

        nominal = self.nominal_map(
            omega
        )

        next_state = (
            nominal
            + control
            + disturbance
        )

        if not math.isfinite(next_state):
            raise FloatingPointError(
                f"Non-finite state generated: {next_state}"
            )

        if next_state <= self.config.plant_minimum:
            raise FloatingPointError(
                f"Plant crossed lower safety bound: {next_state}"
            )

        if next_state >= self.config.plant_maximum:
            raise FloatingPointError(
                f"Plant crossed upper safety bound: {next_state}"
            )

        self.state = next_state

        return next_state


# =============================================================================
# ORACLE
# =============================================================================

class PhiOracle:
    """
    φ-scaled logarithmic observer.

    Λφ(p, Ω)
        = ln(
            p ln(base) / ln(Ω)
          ) / ln(Ω)
          - 1 / (base Ω)

    O
        = 2 |cos(π Λφ / 2)|

    O is bounded in [0, 2].
    """

    def __init__(
        self,
        config: CyberneticConfig,
    ) -> None:

        self.config = config

        if config.base <= 0.0:
            raise ValueError(
                "Oracle base must be positive."
            )

        if config.base == 1.0:
            raise ValueError(
                "Oracle base must not equal 1."
            )

        if config.prime <= 0:
            raise ValueError(
                "Oracle p must be positive."
            )

    def lambda_value(
        self,
        omega: float,
    ) -> float:

        if omega <= 0.0:
            return float("nan")

        ln_base = math.log(
            self.config.base
        )

        ln_omega = math.log(
            omega
        )

        if ln_omega == 0.0:
            return float("nan")

        argument = (
            self.config.prime
            * ln_base
            / ln_omega
        )

        if argument <= 0.0:
            return float("nan")

        value = (
            math.log(argument)
            / ln_omega
            -
            1.0
            /
            (
                self.config.base
                * omega
            )
        )

        return value

    def evaluate(
        self,
        omega: float,
    ) -> float:

        if not self.config.oracle_enabled:
            return 1.0

        lam = self.lambda_value(
            omega
        )

        if not math.isfinite(lam):
            return 1.0

        oracle = (
            2.0
            *
            abs(
                math.cos(
                    math.pi
                    *
                    lam
                    /
                    2.0
                )
            )
        )

        if not math.isfinite(oracle):
            return 1.0

        return max(
            0.0,
            min(
                2.0,
                oracle
            )
        )

    def gain(
        self,
        omega: float,
    ) -> float:

        if not self.config.oracle_enabled:
            return 1.0

        oracle = self.evaluate(
            omega
        )

        value = (
            self.config.oracle_floor
            +
            (
                self.config.oracle_ceiling
                -
                self.config.oracle_floor
            )
            *
            (
                oracle / 2.0
            )
        )

        return value


# =============================================================================
# STATE OBSERVER
# =============================================================================

class StateObserver:
    """
    Estimates:

        Ω
        Ω velocity
        filtered error
        residual
        confidence
    """

    def __init__(
        self,
        reference: float,
        config: CyberneticConfig,
    ) -> None:

        self.reference = reference

        self.config = config

        self.initialized = False

        self.previous_state = reference

        self.velocity = 0.0

        self.filtered_error = 0.0

        self.residual = 0.0

        self.confidence = 1.0

    def reset(
        self,
        state: float,
    ) -> None:

        self.initialized = True

        self.previous_state = state

        self.velocity = 0.0

        self.filtered_error = (
            self.reference - state
        )

        self.residual = 0.0

        self.confidence = 1.0

    def update(
        self,
        state: float,
        expected_nominal: float,
        control: float,
        disturbance: float,
    ) -> Dict[str, float]:

        if not self.initialized:
            self.reset(
                state
            )

        raw_velocity = (
            state
            -
            self.previous_state
        )

        self.velocity = (
            self.config.velocity_alpha
            *
            raw_velocity
            +
            (
                1.0
                -
                self.config.velocity_alpha
            )
            *
            self.velocity
        )

        error = (
            self.reference
            -
            state
        )

        self.filtered_error = (
            self.config.error_alpha
            *
            error
            +
            (
                1.0
                -
                self.config.error_alpha
            )
            *
            self.filtered_error
        )

        predicted_state = (
            expected_nominal
            +
            control
            +
            disturbance
        )

        self.residual = (
            state
            -
            predicted_state
        )

        residual_penalty = min(
            1.0,
            abs(
                self.residual
            )
            /
            max(
                self.config.maximum_residual,
                1.0e-30,
            )
        )

        velocity_penalty = min(
            1.0,
            abs(
                self.velocity
            )
            /
            max(
                self.config.recovery_error_limit,
                1.0e-30,
            )
        )

        self.confidence = max(
            0.0,
            min(
                1.0,
                1.0
                -
                0.5
                *
                residual_penalty
                -
                0.5
                *
                velocity_penalty,
            )
        )

        self.previous_state = state

        return {
            "state": state,
            "velocity": self.velocity,
            "error": error,
            "filtered_error": self.filtered_error,
            "residual": self.residual,
            "confidence": self.confidence,
        }


# =============================================================================
# CONTROLLER TELEMETRY
# =============================================================================

@dataclass
class ControlTerms:
    proportional: float = 0.0
    integral: float = 0.0
    derivative: float = 0.0
    oracle_gain: float = 1.0
    feedback: float = 0.0
    recovery: float = 0.0
    pre_saturation: float = 0.0
    post_saturation: float = 0.0
    slew_limited: bool = False


# =============================================================================
# CYBERNETIC CONTROLLER
# =============================================================================

class CyberneticController:
    """
    Closed-loop controller.

    The control law combines:

        P       = kp * filtered_error
        I       = ki * integral(error)
        D       = kd * (-estimated_velocity)

    then applies the oracle as a gain field:

        oracle_gain = G(O)

    followed by recovery, saturation, and slew limiting.

    The feedback path is:

        measured state
            ↓
        observer
            ↓
        error + velocity + confidence
            ↓
        controller
            ↓
        control
            ↓
        plant
            ↓
        measured state ...
    """

    def __init__(
        self,
        config: CyberneticConfig,
        oracle: PhiOracle,
    ) -> None:

        self.config = config

        self.oracle = oracle

        self.integral = 0.0

        self.previous_control = 0.0

        self.last_terms = ControlTerms()

    def reset(self) -> None:

        self.integral = 0.0

        self.previous_control = 0.0

        self.last_terms = ControlTerms()

    def clamp(
        self,
        value: float,
        low: float,
        high: float,
    ) -> float:

        return max(
            low,
            min(
                high,
                value
            )
        )

    def update(
        self,
        state: float,
        error: float,
        filtered_error: float,
        velocity: float,
        confidence: float,
        omega: float,
    ) -> float:

        cfg = self.config

        # ---------------------------------------------------------------------
        # Deadband
        # ---------------------------------------------------------------------

        effective_error = error

        if abs(
            effective_error
        ) <= cfg.deadband:

            effective_error = 0.0

        # ---------------------------------------------------------------------
        # Integral
        # ---------------------------------------------------------------------

        self.integral += (
            effective_error
        )

        self.integral = self.clamp(
            self.integral,
            -cfg.integral_limit,
            cfg.integral_limit,
        )

        # ---------------------------------------------------------------------
        # PID terms
        # ---------------------------------------------------------------------

        proportional = (
            cfg.kp
            *
            filtered_error
        )

        integral = (
            cfg.ki
            *
            self.integral
        )

        # Negative velocity is a useful direct damping signal:
        #
        #   velocity > 0  => state moving upward
        #   derivative term becomes negative
        #
        derivative = (
            -cfg.kd
            *
            velocity
        )

        base_feedback = (
            proportional
            +
            integral
            +
            derivative
        )

        # ---------------------------------------------------------------------
        # Oracle gain
        # ---------------------------------------------------------------------

        oracle_gain = self.oracle.gain(
            omega
        )

        # Lower confidence reduces the authority of the controller.
        confidence_gain = (
            0.25
            +
            0.75
            *
            confidence
        )

        feedback = (
            base_feedback
            *
            oracle_gain
            *
            confidence_gain
        )

        # ---------------------------------------------------------------------
        # Recovery controller
        # ---------------------------------------------------------------------

        recovery = 0.0

        if abs(
            error
        ) >= cfg.recovery_error_limit:

            recovery = (
                cfg.recovery_gain
                *
                error
            )

            self.integral *= (
                cfg.recovery_integral_scale
            )

        pre_saturation = (
            feedback
            +
            recovery
        )

        # ---------------------------------------------------------------------
        # Actuator saturation
        # ---------------------------------------------------------------------

        saturated = self.clamp(
            pre_saturation,
            -cfg.max_control,
            cfg.max_control,
        )

        # ---------------------------------------------------------------------
        # Slew-rate limiting
        # ---------------------------------------------------------------------

        delta = (
            saturated
            -
            self.previous_control
        )

        slew_limited = False

        if delta > cfg.max_control_delta:

            control = (
                self.previous_control
                +
                cfg.max_control_delta
            )

            slew_limited = True

        elif delta < -cfg.max_control_delta:

            control = (
                self.previous_control
                -
                cfg.max_control_delta
            )

            slew_limited = True

        else:

            control = saturated

        self.previous_control = control

        self.last_terms = ControlTerms(
            proportional=proportional,
            integral=integral,
            derivative=derivative,
            oracle_gain=oracle_gain,
            feedback=feedback,
            recovery=recovery,
            pre_saturation=pre_saturation,
            post_saturation=control,
            slew_limited=slew_limited,
        )

        return control


# =============================================================================
# ROLLING STATISTICS
# =============================================================================

class RollingStatistics:
    def __init__(
        self,
        window: int,
    ) -> None:

        self.window = max(
            1,
            window
        )

        self.errors: Deque[float] = deque(
            maxlen=self.window
        )

        self.controls: Deque[float] = deque(
            maxlen=self.window
        )

        self.oracle: Deque[float] = deque(
            maxlen=self.window
        )

        self.residuals: Deque[float] = deque(
            maxlen=self.window
        )

    def add(
        self,
        error: float,
        control: float,
        oracle: float,
        residual: float,
    ) -> None:

        self.errors.append(
            error
        )

        self.controls.append(
            control
        )

        self.oracle.append(
            oracle
        )

        self.residuals.append(
            residual
        )

    @staticmethod
    def mean(
        values: Deque[float],
    ) -> float:

        if not values:
            return 0.0

        return sum(values) / len(
            values
        )

    @staticmethod
    def rms(
        values: Deque[float],
    ) -> float:

        if not values:
            return 0.0

        return math.sqrt(
            sum(
                value * value
                for value in values
            )
            /
            len(values)
        )

    def summary(self) -> Dict[str, float]:

        return {
            "mean_abs_error":
                self.mean(
                    deque(
                        abs(x)
                        for x in self.errors
                    )
                ),
            "rms_error":
                self.rms(
                    self.errors
                ),
            "mean_control":
                self.mean(
                    self.controls
                ),
            "mean_oracle":
                self.mean(
                    self.oracle
                ),
            "mean_abs_residual":
                self.mean(
                    deque(
                        abs(x)
                        for x in self.residuals
                    )
                ),
        }


# =============================================================================
# TELEMETRY RECORD
# =============================================================================

@dataclass
class TelemetryRecord:
    step: int
    state: float
    reference: float
    error: float
    filtered_error: float
    velocity: float
    residual: float
    confidence: float
    oracle: float
    oracle_gain: float
    proportional: float
    integral: float
    derivative: float
    feedback: float
    recovery: float
    control: float
    disturbance: float
    nominal_state: float
    closed_loop_state: float
    stable: bool
    recovered: bool


# =============================================================================
# FAULT STATE
# =============================================================================

@dataclass
class FaultState:
    faulted: bool = False
    fault_count: int = 0
    last_fault: str = ""


# =============================================================================
# CYBERNETIC ENGINE
# =============================================================================

class CyberneticEngine:
    """
    Complete stateful cybernetic machine.
    """

    def __init__(
        self,
        config: Optional[CyberneticConfig] = None,
    ) -> None:

        self.config = (
            config
            if config is not None
            else CyberneticConfig()
        )

        self.disturbance_source = (
            DisturbanceSource(
                self.config
            )
        )

        initial_state = (
            self.config.reference
            +
            self.config.initial_offset
        )

        self.plant = GoldenPlant(
            initial_state,
            self.config,
        )

        self.oracle = PhiOracle(
            self.config
        )

        self.observer = StateObserver(
            self.config.reference,
            self.config,
        )

        self.controller = CyberneticController(
            self.config,
            self.oracle,
        )

        self.statistics = RollingStatistics(
            self.config.telemetry_window
        )

        self.telemetry: List[
            TelemetryRecord
        ] = []

        self.fault = FaultState()

        self.running = True

        self.settled_count = 0

        self.first_settled_step: Optional[
            int
        ] = None

        self.total_abs_error = 0.0

        self.total_squared_error = 0.0

        self.maximum_abs_error = 0.0

        self.total_control_effort = 0.0

        self.total_disturbance_energy = 0.0

        self.controller.reset()

    # -------------------------------------------------------------------------
    # Stop
    # -------------------------------------------------------------------------

    def stop(self) -> None:

        self.running = False

    # -------------------------------------------------------------------------
    # Fault handling
    # -------------------------------------------------------------------------

    def register_fault(
        self,
        message: str,
    ) -> None:

        self.fault.faulted = True

        self.fault.fault_count += 1

        self.fault.last_fault = message

    def clear_fault(self) -> None:

        self.fault.faulted = False

        self.fault.last_fault = ""

    def recover(
        self,
    ) -> None:

        """
        Controlled recovery.

        Reset controller memory while preserving the plant.
        """

        self.controller.reset()

        self.observer.reset(
            self.plant.state
        )

        self.clear_fault()

    # -------------------------------------------------------------------------
    # Stability
    # -------------------------------------------------------------------------

    def is_stable(
        self,
        error: float,
        residual: float,
    ) -> bool:

        if not math.isfinite(error):
            return False

        if not math.isfinite(residual):
            return False

        if abs(error) > self.config.divergence_limit:
            return False

        if abs(residual) > self.config.maximum_residual:
            return False

        if self.plant.state <= self.config.plant_minimum:
            return False

        if self.plant.state >= self.config.plant_maximum:
            return False

        return True

    # -------------------------------------------------------------------------
    # Settling
    # -------------------------------------------------------------------------

    def update_settling(
        self,
        step: int,
        error: float,
    ) -> None:

        if (
            abs(error)
            <= self.config.settling_tolerance
        ):

            self.settled_count += 1

            if (
                self.first_settled_step
                is None
            ):

                if (
                    self.settled_count
                    >= self.config.settling_window
                ):

                    self.first_settled_step = (
                        step
                        -
                        self.config.settling_window
                        +
                        1
                    )

        else:

            self.settled_count = 0

    # -------------------------------------------------------------------------
    # Single cybernetic cycle
    # -------------------------------------------------------------------------

    def step(
        self,
        step: int,
    ) -> TelemetryRecord:

        previous_state = (
            self.plant.state
        )

        # ---------------------------------------------------------------------
        # Disturbance
        # ---------------------------------------------------------------------

        disturbance = (
            self.disturbance_source.next()
        )

        # ---------------------------------------------------------------------
        # Oracle
        # ---------------------------------------------------------------------

        oracle_value = (
            self.oracle.evaluate(
                previous_state
            )
        )

        oracle_gain = (
            self.oracle.gain(
                previous_state
            )
        )

        # ---------------------------------------------------------------------
        # Nominal plant prediction
        # ---------------------------------------------------------------------

        nominal_state = (
            self.plant.nominal_map(
                previous_state
            )
        )

        # ---------------------------------------------------------------------
        # Preliminary observation
        # ---------------------------------------------------------------------

        predicted_without_control = (
            nominal_state
            +
            disturbance
        )

        estimated_velocity = (
            self.observer.velocity
        )

        error = (
            self.config.reference
            -
            previous_state
        )

        observer_data = (
            self.observer.update(
                state=previous_state,
                expected_nominal=nominal_state,
                control=self.controller.previous_control,
                disturbance=disturbance,
            )
        )

        # Replace raw values with filtered observer values.
        filtered_error = (
            observer_data[
                "filtered_error"
            ]
        )

        velocity = (
            observer_data[
                "velocity"
            ]
        )

        confidence = (
            observer_data[
                "confidence"
            ]
        )

        # ---------------------------------------------------------------------
        # Controller
        # ---------------------------------------------------------------------

        control = (
            self.controller.update(
                state=previous_state,
                error=error,
                filtered_error=filtered_error,
                velocity=velocity,
                confidence=confidence,
                omega=previous_state,
            )
        )

        # ---------------------------------------------------------------------
        # Plant update
        # ---------------------------------------------------------------------

        try:

            closed_loop_state = (
                self.plant.update(
                    control,
                    disturbance,
                )
            )

        except (
            FloatingPointError,
            ZeroDivisionError,
        ) as exc:

            self.register_fault(
                str(exc)
            )

            # Hold the current state if possible.
            closed_loop_state = (
                previous_state
            )

            self.plant.state = (
                previous_state
            )

        # ---------------------------------------------------------------------
        # Actual residual
        # ---------------------------------------------------------------------

        actual_residual = (
            closed_loop_state
            -
            (
                nominal_state
                +
                control
                +
                disturbance
            )
        )

        # ---------------------------------------------------------------------
        # Error after plant transition
        # ---------------------------------------------------------------------

        next_error = (
            self.config.reference
            -
            closed_loop_state
        )

        recovered = False

        # ---------------------------------------------------------------------
        # Stability
        # ---------------------------------------------------------------------

        stable = self.is_stable(
            next_error,
            actual_residual,
        )

        if not stable:

            self.register_fault(
                "closed-loop stability boundary exceeded"
            )

            self.recover()

            recovered = True

            stable = True

        # ---------------------------------------------------------------------
        # Aggregate statistics
        # ---------------------------------------------------------------------

        self.total_abs_error += abs(
            error
        )

        self.total_squared_error += (
            error * error
        )

        self.maximum_abs_error = max(
            self.maximum_abs_error,
            abs(error)
        )

        self.total_control_effort += (
            abs(control)
        )

        self.total_disturbance_energy += (
            disturbance * disturbance
        )

        self.statistics.add(
            error=error,
            control=control,
            oracle=oracle_value,
            residual=actual_residual,
        )

        self.update_settling(
            step,
            next_error,
        )

        terms = (
            self.controller.last_terms
        )

        record = TelemetryRecord(
            step=step,
            state=previous_state,
            reference=self.config.reference,
            error=error,
            filtered_error=filtered_error,
            velocity=(
                velocity
                if math.isfinite(
                    velocity
                )
                else estimated_velocity
            ),
            residual=actual_residual,
            confidence=confidence,
            oracle=oracle_value,
            oracle_gain=oracle_gain,
            proportional=terms.proportional,
            integral=terms.integral,
            derivative=terms.derivative,
            feedback=terms.feedback,
            recovery=terms.recovery,
            control=control,
            disturbance=disturbance,
            nominal_state=nominal_state,
            closed_loop_state=closed_loop_state,
            stable=stable,
            recovered=recovered,
        )

        self.telemetry.append(
            record
        )

        return record

    # -------------------------------------------------------------------------
    # Console
    # -------------------------------------------------------------------------

    def print_header(self) -> None:

        print(
            "=" * 124
        )

        print(
            " शून्यत्वम् — FULL CYBERNETIC ENGINE"
        )

        print(
            "=" * 124
        )

        print(
            f"φ              = {PHI:.15f}"
        )

        print(
            f"ψ              = {PHI_CONJUGATE:.15f}"
        )

        print(
            f"1/φ            = {PHI_RECIPROCAL:.15f}"
        )

        print(
            f"plant derivative= {PHI_MAP_DERIVATIVE:.15f}"
        )

        print(
            f"initial Ω       = "
            f"{self.plant.state:.15f}"
        )

        print(
            f"reference       = "
            f"{self.config.reference:.15f}"
        )

        print(
            f"oracle p        = "
            f"{self.config.prime}"
        )

        print(
            f"oracle base     = "
            f"{self.config.base}"
        )

        print(
            f"steps           = "
            f"{self.config.steps}"
        )

        print(
            f"disturbance     = "
            f"±{self.config.disturbance_amplitude:.3e}"
        )

        print(
            f"oracle          = "
            f"{'ON' if self.config.oracle_enabled else 'OFF'}"
        )

        print()

        print(
            f"{'STEP':>8}"
            f"{'Ω':>18}"
            f"{'ERROR':>16}"
            f"{'VELO':>14}"
            f"{'ORACLE':>12}"
            f"{'GAIN':>10}"
            f"{'CONTROL':>14}"
            f"{'CONF':>10}"
            f"{'RESID':>14}"
            f"{'STATE':>12}"
        )

        print(
            "-" * 124
        )

    def print_record(
        self,
        record: TelemetryRecord,
    ) -> None:

        state = (
            "OK"
            if record.stable
            else "FAULT"
        )

        if record.recovered:
            state = "RECOVER"

        print(
            f"{record.step:>8}"
            f"{record.state:>18.12f}"
            f"{record.error:>+16.6e}"
            f"{record.velocity:>+14.6e}"
            f"{record.oracle:>12.8f}"
            f"{record.oracle_gain:>10.6f}"
            f"{record.control:>+14.6e}"
            f"{record.confidence:>10.6f}"
            f"{record.residual:>+14.6e}"
            f"{state:>12}"
        )

    # -------------------------------------------------------------------------
    # Run
    # -------------------------------------------------------------------------

    def run(self) -> None:

        self.print_header()

        for step in range(
            self.config.steps
        ):

            if not self.running:
                break

            record = self.step(
                step
            )

            if (
                step % self.config.print_every
                == 0
            ):

                self.print_record(
                    record
                )

        print()

        self.print_summary()

    # -------------------------------------------------------------------------
    # Summary
    # -------------------------------------------------------------------------

    def summary(self) -> Dict[str, object]:

        count = len(
            self.telemetry
        )

        if count == 0:
            return {
                "steps": 0,
                "error": None,
            }

        rms = math.sqrt(
            self.total_squared_error
            /
            count
        )

        mae = (
            self.total_abs_error
            /
            count
        )

        final_state = (
            self.plant.state
        )

        final_error = (
            self.config.reference
            -
            final_state
        )

        recent = (
            self.statistics.summary()
        )

        return {
            "engine": "शून्यत्वम्",
            "architecture": "closed-loop cybernetic controller",
            "steps": count,
            "reference_phi": self.config.reference,
            "initial_state": (
                self.config.reference
                +
                self.config.initial_offset
            ),
            "final_state": final_state,
            "final_error": final_error,
            "mean_absolute_error": mae,
            "root_mean_square_error": rms,
            "maximum_absolute_error": (
                self.maximum_abs_error
            ),
            "total_control_effort": (
                self.total_control_effort
            ),
            "disturbance_energy": (
                self.total_disturbance_energy
            ),
            "settling_step": (
                self.first_settled_step
            ),
            "fault_count": (
                self.fault.fault_count
            ),
            "last_fault": (
                self.fault.last_fault
            ),
            "rolling": recent,
        }

    def print_summary(self) -> None:

        summary = self.summary()

        print(
            "=" * 78
        )

        print(
            " CYBERNETIC STATE SUMMARY"
        )

        print(
            "=" * 78
        )

        print(
            f"steps              : "
            f"{summary.get('steps')}"
        )

        print(
            f"reference φ        : "
            f"{summary.get('reference_phi'):.15f}"
        )

        print(
            f"final Ω            : "
            f"{summary.get('final_state'):.15f}"
        )

        print(
            f"final error        : "
            f"{summary.get('final_error'):+.12e}"
        )

        print(
            f"MAE                : "
            f"{summary.get('mean_absolute_error'):.12e}"
        )

        print(
            f"RMSE               : "
            f"{summary.get('root_mean_square_error'):.12e}"
        )

        print(
            f"maximum error      : "
            f"{summary.get('maximum_absolute_error'):.12e}"
        )

        print(
            f"control effort     : "
            f"{summary.get('total_control_effort'):.12e}"
        )

        print(
            f"disturbance energy : "
            f"{summary.get('disturbance_energy'):.12e}"
        )

        settling = (
            summary.get(
                "settling_step"
            )
        )

        if settling is None:

            print(
                "settling           : NOT ESTABLISHED"
            )

        else:

            print(
                f"settling step      : "
                f"{settling}"
            )

        print(
            f"fault count        : "
            f"{summary.get('fault_count')}"
        )

        if summary.get(
            "last_fault"
        ):

            print(
                f"last fault         : "
                f"{summary.get('last_fault')}"
            )

        rolling = summary.get(
            "rolling",
            {}
        )

        print()

        print(
            "ROLLING WINDOW"
        )

        print(
            f"mean |error|       : "
            f"{rolling.get('mean_abs_error', 0.0):.12e}"
        )

        print(
            f"RMS error          : "
            f"{rolling.get('rms_error', 0.0):.12e}"
        )

        print(
            f"mean control       : "
            f"{rolling.get('mean_control', 0.0):+.12e}"
        )

        print(
            f"mean oracle        : "
            f"{rolling.get('mean_oracle', 0.0):.12e}"
        )

        print(
            f"mean |residual|    : "
            f"{rolling.get('mean_abs_residual', 0.0):.12e}"
        )

        print()

    # -------------------------------------------------------------------------
    # CSV
    # -------------------------------------------------------------------------

    def write_csv(
        self,
        path: str,
    ) -> None:

        if not self.telemetry:
            return

        output = Path(
            path
        )

        fields = list(
            asdict(
                self.telemetry[0]
            ).keys()
        )

        with output.open(
            "w",
            newline="",
            encoding="utf-8",
        ) as handle:

            writer = csv.DictWriter(
                handle,
                fieldnames=fields,
            )

            writer.writeheader()

            for record in self.telemetry:

                writer.writerow(
                    asdict(record)
                )

    # -------------------------------------------------------------------------
    # JSON
    # -------------------------------------------------------------------------

    def write_json(
        self,
        path: str,
    ) -> None:

        output = Path(
            path
        )

        payload = {
            "configuration": asdict(
                self.config
            ),
            "summary": self.summary(),
        }

        with output.open(
            "w",
            encoding="utf-8",
        ) as handle:

            json.dump(
                payload,
                handle,
                indent=2,
            )

            handle.write("\n")

    # -------------------------------------------------------------------------
    # Files
    # -------------------------------------------------------------------------

    def export(
        self,
    ) -> None:

        if not self.config.write_files:
            return

        self.write_csv(
            self.config.csv_path
        )

        self.write_json(
            self.config.json_path
        )


# =============================================================================
# SIGNAL HANDLING
# =============================================================================

_ENGINE: Optional[
    CyberneticEngine
] = None


def handle_signal(
    signum: int,
    frame,
) -> None:

    del frame

    if _ENGINE is not None:

        print()

        print(
            f"[signal {signum}] shutdown requested"
        )

        _ENGINE.stop()


# =============================================================================
# MAIN
# =============================================================================

def main() -> int:

    global _ENGINE

    config = CyberneticConfig()

    _ENGINE = CyberneticEngine(
        config
    )

    signal.signal(
        signal.SIGINT,
        handle_signal
    )

    if hasattr(
        signal,
        "SIGTERM"
    ):

        signal.signal(
            signal.SIGTERM,
            handle_signal
        )

    start = time.perf_counter()

    try:

        _ENGINE.run()

    except KeyboardInterrupt:

        print()
        print(
            "Keyboard interrupt."
        )

        _ENGINE.stop()

    except Exception as exc:

        print()
        print(
            "=" * 78
        )

        print(
            "CYBERNETIC ENGINE FAULT"
        )

        print(
            "=" * 78
        )

        print(
            f"{type(exc).__name__}: {exc}"
        )

        _ENGINE.register_fault(
            str(exc)
        )

        _ENGINE.stop()

    finally:

        _ENGINE.export()

    elapsed = (
        time.perf_counter()
        -
        start
    )

    print()

    print(
        f"runtime            : "
        f"{elapsed:.6f} s"
    )

    print(
        f"rate               : "
        f"{len(_ENGINE.telemetry) / elapsed:.3f} cycles/s"
        if elapsed > 0.0
        else "rate               : n/a"
    )

    print()

    print(
        "CYBERNETIC ENGINE CLOSED."
    )

    return 0


# =============================================================================
# ENTRY
# =============================================================================

if __name__ == "__main__":
    raise SystemExit(
        main()
    )

YIELDS:

============================================================================================================================

 शून्यत्वम् — FULL CYBERNETIC ENGINE

============================================================================================================================

φ              = 1.618033988749895

ψ              = -0.618033988749895

1/φ            = 0.618033988749895

plant derivative= -0.381966011250105

initial Ω       = 1.628033988749895

reference       = 1.618033988749895

oracle p        = 7

oracle base     = 10.0

steps           = 10000

disturbance     = ±1.000e-06

oracle          = ON

1680 |

    STEP                 Ω           ERROR          VELO      ORACLE      GAIN       CONTROL      CONF         RESID       STATE

----------------------------------------------------------------------------------------------------------------------------

       0    1.628033988750   -1.000000e-02 +0.000000e+00  0.36611448  0.683057 -2.412308e-03  0.993102 +0.000000e+00          OK

      10    1.617882121160   +1.518676e-04 -1.012316e-04  0.72746093  0.863730 -1.766889e-04  0.999483 +0.000000e+00          OK

      20    1.618024750170   +9.238580e-06 +1.707516e-06  0.72244718  0.861224 -9.924932e-06  0.999991 +0.000000e+00          OK

      30    1.618033897861   +9.088935e-08 +4.129443e-07  0.72212553  0.861063 +1.353406e-06  0.999997 +0.000000e+00          OK

      40    1.618034803645   -8.148950e-07 -1.102062e-07  0.72209368  0.861047 +1.965216e-06  0.999999 +0.000000e+00          OK

      50    1.618035521031   -1.532281e-06 +1.109335e-08  0.72206845  0.861034 +1.909325e-06  1.000000 +0.000000e+00          OK

      60    1.618036383867   -2.395117e-06 +2.800561e-07  0.72203811  0.861019 +1.823983e-06  0.999998 +0.000000e+00          OK

      70    1.618035791821   -1.803071e-06 +1.153764e-07  0.72205893  0.861029 +1.807200e-06  0.999999 +0.000000e+00          OK

      80    1.618035150231   -1.161481e-06 -9.423201e-08  0.72208149  0.861041 +1.764688e-06  0.999999 +0.000000e+00          OK

      90    1.618036636482   -2.647732e-06 +3.879873e-07  0.72202923  0.861015 +1.664028e-06  0.999998 +0.000000e+00          OK

     100    1.618034378918   -3.901685e-07 -2.660513e-07  0.72210861  0.861054 +1.722745e-06  0.999998 +0.000000e+00          OK

     110    1.618035815878   -1.827128e-06 +9.458291e-08  0.72205808  0.861029 +1.554069e-06  0.999999 +0.000000e+00          OK

     120    1.618036018106   -2.029356e-06 +2.020903e-07  0.72205097  0.861025 +1.517046e-06  0.999998 +0.000000e+00          OK

     130    1.618035236999   -1.248249e-06 +6.921757e-09  0.72207844  0.861039 +1.540245e-06  1.000000 +0.000000e+00          OK

     140    1.618035268828   -1.280079e-06 +4.668342e-08  0.72207732  0.861039 +1.508824e-06  1.000000 +0.000000e+00          OK

     150    1.618034781639   -7.928891e-07 -5.374994e-08  0.72209445  0.861047 +1.524991e-06  1.000000 +0.000000e+00          OK

     160    1.618035658190   -1.669440e-06 +2.000255e-07  0.72206363  0.861032 +1.442245e-06  0.999998 +0.000000e+00          OK

     170    1.618034102363   -1.136131e-07 -2.585922e-07  0.72211834  0.861059 +1.477687e-06  0.999998 +0.000000e+00          OK

     180    1.618033460754   +5.279960e-07 -4.348054e-07  0.72214090  0.861070 +1.473769e-06  0.999997 +0.000000e+00          OK

     190    1.618034299664   -3.109143e-07 -1.902921e-07  0.72211140  0.861056 +1.395334e-06  0.999999 +0.000000e+00          OK

     200    1.618034040574   -5.182364e-08 -2.561842e-07  0.72212051  0.861060 +1.368642e-06  0.999998 +0.000000e+00          OK

     210    1.618034276311   -2.875607e-07 -2.166060e-07  0.72211222  0.861056 +1.291997e-06  0.999998 +0.000000e+00          OK

     220    1.618035547083   -1.558333e-06 +2.008410e-07  0.72206754  0.861034 +1.218056e-06  0.999999 +0.000000e+00          OK

     230    1.618034433099   -4.443494e-07 -1.699207e-07  0.72210671  0.861053 +1.196709e-06  0.999999 +0.000000e+00          OK

     240    1.618035121843   -1.133093e-06 +1.118085e-10  0.72208249  0.861041 +1.091444e-06  1.000000 +0.000000e+00          OK

     250    1.618035216557   -1.227807e-06 +1.167652e-07  0.72207916  0.861040 +1.116223e-06  0.999999 +0.000000e+00          OK

     260    1.618036049113   -2.060363e-06 +3.601348e-07  0.72204988  0.861025 +1.045649e-06  0.999998 +0.000000e+00          OK

     270    1.618034942692   -9.539418e-07 +6.673981e-08  0.72208879  0.861044 +1.083012e-06  0.999999 +0.000000e+00          OK

     280    1.618035385160   -1.396410e-06 +1.755651e-07  0.72207323  0.861037 +1.012060e-06  0.999999 +0.000000e+00          OK

     290    1.618034301588   -3.128385e-07 -1.759310e-07  0.72211133  0.861056 +1.013081e-06  0.999999 +0.000000e+00          OK

     300    1.618035381868   -1.393118e-06 +1.315120e-07  0.72207335  0.861037 +9.208978e-07  0.999999 +0.000000e+00          OK

     310    1.618033816121   +1.726286e-07 -2.193067e-07  0.72212840  0.861064 +1.038512e-06  0.999998 +0.000000e+00          OK

     320    1.618034780030   -7.912803e-07 +7.395703e-08  0.72209451  0.861047 +9.700307e-07  0.999999 +0.000000e+00          OK

     330    1.618034588828   -6.000780e-07 -1.205429e-08  0.72210123  0.861051 +9.419302e-07  1.000000 +0.000000e+00          OK

     340    1.618034091148   -1.023986e-07 -1.542731e-07  0.72211873  0.861059 +9.370565e-07  0.999999 +0.000000e+00          OK

     350    1.618034717974   -7.292239e-07 -1.158505e-08  0.72209669  0.861048 +8.379068e-07  1.000000 +0.000000e+00          OK

     360    1.618035493285   -1.504535e-06 +1.812869e-07  0.72206943  0.861035 +7.375655e-07  0.999999 +0.000000e+00          OK

     370    1.618034611903   -6.231530e-07 -3.226268e-08  0.72210042  0.861050 +7.824481e-07  1.000000 +0.000000e+00          OK

     380    1.618035673198   -1.684448e-06 +3.398384e-07  0.72206310  0.861032 +7.646916e-07  0.999997 +0.000000e+00          OK

     390    1.618033796550   +1.922001e-07 -1.701475e-07  0.72212909  0.861065 +8.696278e-07  0.999999 +0.000000e+00          OK

     400    1.618034924989   -9.362389e-07 +7.553275e-08  0.72208941  0.861045 +7.169641e-07  0.999999 +0.000000e+00          OK

     410    1.618034261023   -2.722729e-07 -5.503312e-08  0.72211276  0.861056 +7.731800e-07  0.999999 +0.000000e+00          OK

     420    1.618035288251   -1.299501e-06 +1.500150e-07  0.72207664  0.861038 +6.338718e-07  0.999998 +0.000000e+00          OK

     430    1.618033890787   +9.796323e-08 -1.764282e-07  0.72212578  0.861063 +7.373199e-07  0.999999 +0.000000e+00          OK

     440    1.618033273925   +7.148250e-07 -3.393207e-07  0.72214747  0.861074 +7.605828e-07  0.999997 +0.000000e+00          OK

     450    1.618034448315   -4.595653e-07 -4.442432e-08  0.72210617  0.861053 +6.383789e-07  1.000000 +0.000000e+00          OK

     460    1.618033883935   +1.048150e-07 -1.507130e-07  0.72212602  0.861063 +6.889001e-07  0.999999 +0.000000e+00          OK

     470    1.618035647745   -1.658995e-06 +3.457911e-07  0.72206400  0.861032 +5.752996e-07  0.999997 +0.000000e+00          OK

     480    1.618033716453   +2.722965e-07 -1.711093e-07  0.72213191  0.861066 +6.876486e-07  0.999999 +0.000000e+00          OK

     490    1.618035697911   -1.709161e-06 +3.670308e-07  0.72206223  0.861031 +5.393455e-07  0.999997 +0.000000e+00          OK

     500    1.618033173251   +8.154993e-07 -3.489772e-07  0.72215101  0.861076 +6.659312e-07  0.999998 +0.000000e+00          OK

     510    1.618034573002   -5.842523e-07 +8.331541e-08  0.72210179  0.861051 +5.983886e-07  0.999999 +0.000000e+00          OK

     520    1.618035634325   -1.645575e-06 +3.696898e-07  0.72206447  0.861032 +5.064198e-07  0.999997 +0.000000e+00          OK

     530    1.618035508081   -1.519331e-06 +2.867966e-07  0.72206891  0.861034 +4.586143e-07  0.999998 +0.000000e+00          OK

     540    1.618034736533   -7.477832e-07 +7.714920e-08  0.72209604  0.861048 +4.941314e-07  0.999999 +0.000000e+00          OK

     550    1.618034327371   -3.386213e-07 +3.857820e-08  0.72211043  0.861055 +5.595304e-07  1.000000 +0.000000e+00          OK

     560    1.618033886443   +1.023066e-07 -8.818508e-08  0.72212593  0.861063 +5.673949e-07  0.999999 +0.000000e+00          OK

     570    1.618034310844   -3.220941e-07 -5.203584e-08  0.72211101  0.861056 +4.649361e-07  1.000000 +0.000000e+00          OK

     580    1.618034079135   -9.038499e-08 +1.796466e-08  0.72211915  0.861060 +5.739673e-07  1.000000 +0.000000e+00          OK

     590    1.618033929018   +5.973227e-08 -1.429045e-07  0.72212443  0.861062 +4.739325e-07  0.999999 +0.000000e+00          OK

     600    1.618034298742   -3.099924e-07 -4.665615e-08  0.72211143  0.861056 +4.225965e-07  0.999999 +0.000000e+00          OK

     610    1.618035037060   -1.048310e-06 +1.667423e-07  0.72208547  0.861043 +3.642208e-07  0.999999 +0.000000e+00          OK

     620    1.618034750708   -7.619579e-07 +1.081236e-07  0.72209554  0.861048 +3.790618e-07  0.999999 +0.000000e+00          OK

     630    1.618034772458   -7.837079e-07 +5.294139e-08  0.72209477  0.861047 +3.140603e-07  0.999999 +0.000000e+00          OK

     640    1.618035404861   -1.416112e-06 +3.018858e-07  0.72207254  0.861036 +3.207236e-07  0.999998 +0.000000e+00          OK

     650    1.618034614359   -6.256096e-07 +5.330620e-08  0.72210033  0.861050 +3.200979e-07  0.999999 +0.000000e+00          OK

     660    1.618033899614   +8.913581e-08 -8.581012e-08  0.72212547  0.861063 +3.992822e-07  1.000000 +0.000000e+00          OK

     670    1.618033012186   +9.765638e-07 -3.509831e-07  0.72215667  0.861078 +4.257759e-07  0.999997 +0.000000e+00          OK

     680    1.618033961030   +2.772028e-08 -9.636818e-08  0.72212331  0.861062 +3.518382e-07  0.999999 +0.000000e+00          OK

     690    1.618034321872   -3.331222e-07 +1.016892e-07  0.72211062  0.861055 +4.037608e-07  0.999999 +0.000000e+00          OK

     700    1.618033759267   +2.294828e-07 -7.890045e-08  0.72213040  0.861065 +4.058919e-07  0.999999 +0.000000e+00          OK

     710    1.618034699288   -7.105383e-07 +1.863124e-07  0.72209735  0.861049 +3.503712e-07  0.999998 +0.000000e+00          OK

     720    1.618034785661   -7.969115e-07 +1.417808e-07  0.72209431  0.861047 +2.910946e-07  0.999999 +0.000000e+00          OK

     730    1.618032905378   +1.083372e-06 -3.561440e-07  0.72216043  0.861080 +4.228797e-07  0.999998 +0.000000e+00          OK

     740    1.618033865839   +1.229106e-07 -9.874372e-08  0.72212665  0.861063 +3.469317e-07  0.999999 +0.000000e+00          OK

     750    1.618034807204   -8.184538e-07 +1.609057e-07  0.72209355  0.861047 +2.649488e-07  0.999999 +0.000000e+00          OK

     760    1.618034726541   -7.377906e-07 +1.568518e-07  0.72209639  0.861048 +2.732415e-07  0.999999 +0.000000e+00          OK

     770    1.618034055768   -6.701784e-08 -8.530877e-08  0.72211998  0.861060 +2.698243e-07  0.999999 +0.000000e+00          OK

     780    1.618035143570   -1.154820e-06 +2.345459e-07  0.72208173  0.861041 +2.045242e-07  0.999998 +0.000000e+00          OK

     790    1.618033912948   +7.580223e-08 -5.282160e-08  0.72212500  0.861062 +3.078918e-07  0.999999 +0.000000e+00          OK

     800    1.618033848669   +1.400813e-07 -1.001715e-07  0.72212726  0.861064 +2.783650e-07  0.999999 +0.000000e+00          OK

     810    1.618033511674   +4.770756e-07 -1.513814e-07  0.72213911  0.861070 +3.368584e-07  0.999999 +0.000000e+00          OK

     820    1.618034590240   -6.014898e-07 +7.969479e-08  0.72210118  0.861051 +2.001166e-07  0.999999 +0.000000e+00          OK

     830    1.618034418503   -4.297526e-07 +4.178802e-08  0.72210722  0.861054 +2.125162e-07  1.000000 +0.000000e+00          OK

     840    1.618033108136   +8.806136e-07 -2.974900e-07  0.72215330  0.861077 +3.052529e-07  0.999998 +0.000000e+00          OK

     850    1.618033440207   +5.485433e-07 -1.598396e-07  0.72214162  0.861071 +3.161578e-07  0.999999 +0.000000e+00          OK

     860    1.618034752964   -7.642146e-07 +1.134105e-07  0.72209546  0.861048 +1.476903e-07  0.999999 +0.000000e+00          OK

     870    1.618034731967   -7.432175e-07 +1.109826e-07  0.72209620  0.861048 +1.468426e-07  0.999999 +0.000000e+00          OK

     880    1.618033470461   +5.182886e-07 -1.580710e-07  0.72214056  0.861070 +2.744067e-07  0.999999 +0.000000e+00          OK

     890    1.618033924037   +6.471274e-08 -3.846549e-08  0.72212461  0.861062 +2.375536e-07  1.000000 +0.000000e+00          OK

     900    1.618034357893   -3.691428e-07 +2.211595e-08  0.72210935  0.861055 +1.704644e-07  1.000000 +0.000000e+00          OK

     910    1.618034426841   -4.380915e-07 +5.293526e-08  0.72210693  0.861053 +1.444293e-07  0.999999 +0.000000e+00          OK

     920    1.618034553332   -5.645824e-07 +1.282641e-07  0.72210248  0.861051 +1.753581e-07  0.999999 +0.000000e+00          OK

     930    1.618033310476   +6.782744e-07 -2.067428e-07  0.72214618  0.861073 +2.434885e-07  0.999999 +0.000000e+00          OK

     940    1.618034022435   -3.368467e-08 +3.663825e-08  0.72212115  0.861061 +2.427282e-07  1.000000 +0.000000e+00          OK

     950    1.618034362394   -3.736439e-07 +3.572174e-08  0.72210919  0.861055 +1.403705e-07  0.999999 +0.000000e+00          OK

     960    1.618034473565   -4.848155e-07 -4.887119e-09  0.72210528  0.861053 +5.766932e-08  1.000000 +0.000000e+00          OK

     970    1.618033651783   +3.369670e-07 -1.399700e-07  0.72213418  0.861067 +1.632620e-07  0.999999 +0.000000e+00          OK

     980    1.618034762830   -7.740803e-07 +1.677530e-07  0.72209511  0.861048 +8.982894e-08  0.999999 +0.000000e+00          OK

     990    1.618034011206   -2.245611e-08 -5.400344e-08  0.72212154  0.861061 +1.262681e-07  1.000000 +0.000000e+00          OK

    1000    1.618034185334   -1.965840e-07 +2.253024e-09  0.72211542  0.861058 +1.134160e-07  0.999999 +0.000000e+00          OK

    1010    1.618034141501   -1.527513e-07 +1.019551e-07  0.72211696  0.861058 +2.124959e-07  0.999999 +0.000000e+00          OK

    1020    1.618034419191   -4.304414e-07 +8.548929e-08  0.72210720  0.861054 +1.277617e-07  0.999999 +0.000000e+00          OK

Combined-asm

; =============================================================================
; HDGL — REAL CYBERNETIC CORE
; =============================================================================
;
; CLOSED-LOOP Z[φ] CYBERNETIC SUBSTRATE
;
; BUILD:
;   nasm -f bin hdgl_cybernetic_core.asm -o hdgl_cybernetic_core.img
;
; RUN:
;   qemu-system-x86_64 -drive format=raw,file=hdgl_cybernetic_core.img -m 128M -smp 1 -boot c
;
; -----------------------------------------------------------------------------
; CORE IDEA
; -----------------------------------------------------------------------------
;
; This is no longer a passive observer.
;
; The machine performs:
;
;     OBSERVE
;       ↓
;     SCORE CANDIDATE CORRECTIONS
;       ↓
;     SELECT CONTROL
;       ↓
;     APPLY CONTROL TO INPUT STATE
;       ↓
;     FIRE
;       ↓
;     WATER VERIFY
;       ↓
;     EARTH VERIFY
;       ↓
;     WIND MEASURE
;       ↓
;     COMMIT
;       ↓
;     REPEAT
;
; The controller is a one-step discrete model-predictive controller.
;
; Current state:
;
;     X = (a,b) ∈ Z²
;
; FIRE:
;
;     F(a,b) = (a+b,a)
;
; WIND:
;
;     T(X) = 1 + 1/X
;
;     fixed-point residual in Z[φ]:
;
;       Rφ = a² + 2ab - a
;       Rc = a² + b² - b - 1
;
; EARTH:
;
;     Nφ(a,b) = -a² + ab + b²
;
; WATER:
;
;     W(a,b) = (b,a-b)
;
;     W(F(a,b)) = (a,b)
;
; CONTROLLER:
;
;     Examine a finite neighborhood of the current state:
;
;         ( a-1, b-1 )
;         ( a-1, b   )
;         ( a-1, b+1 )
;         ( a,   b-1 )
;         ( a,   b   )
;         ( a,   b+1 )
;         ( a+1, b-1 )
;         ( a+1, b   )
;         ( a+1, b+1 )
;
;     For each candidate:
;
;         1. Apply FIRE.
;         2. Compute WIND residual of the predicted state.
;         3. Compute EARTH invariant error.
;         4. Reject candidates that fail WATER consistency.
;         5. Select the minimum-cost candidate.
;
;     The selected candidate becomes the actual actuator input.
;
; Thus STRATEGY is no longer merely a label:
;
;     CONTROL_A / CONTROL_B
;
; actually changes the state trajectory.
;
; -----------------------------------------------------------------------------
; NO:
;     libc
;     BIOS after long mode
;     floating point
;     SSE
;     AVX
;     FPU
;     division
;     multiplication by arbitrary constants in the controller
;
; Integer MUL is used only for algebraic observer calculations.
;
; =============================================================================


BITS 16
ORG 0x7C00


; =============================================================================
; BOOT CONSTANTS
; =============================================================================

IMAGE_SECTORS      equ 48
PAYLOAD_SECTORS    equ IMAGE_SECTORS - 1

LOAD_SEG           equ 0x07E0
LOAD_PHYS          equ 0x00007E00

PAGE_PML4          equ 0x00021000
PAGE_PDPT          equ 0x00022000
PAGE_PD0           equ 0x00023000
PAGE_PD1           equ 0x00024000
PAGE_PD2           equ 0x00025000
PAGE_PD3           equ 0x00026000

BSP_STACK          equ 0x00070000

VGA_BASE           equ 0x000B8000
VGA_ROW_BYTES      equ 160

PRINT_EVERY        equ 65536
PRINT_MASK         equ PRINT_EVERY - 1


; =============================================================================
; SHARED CYBERNETIC STATE
; =============================================================================

STATE_A            equ 0x00500000
STATE_B            equ 0x00500008
STATE_K            equ 0x00500010

; Controlled input state selected by the controller.
CONTROL_A          equ 0x00500020
CONTROL_B          equ 0x00500028

; FIRE output.
FIRE_A             equ 0x00500030
FIRE_B             equ 0x00500038

; WATER verification.
WATER_A            equ 0x00500040
WATER_B            equ 0x00500048
WATER_OK           equ 0x00500050

; EARTH observer.
EARTH_N            equ 0x00500060
EARTH_N_FIRE       equ 0x00500068
EARTH_DELTA        equ 0x00500070
EARTH_COST         equ 0x00500078

; WIND observer.
WIND_RES_A         equ 0x00500080
WIND_RES_B         equ 0x00500088
WIND_COST          equ 0x00500090
WIND_FIXED         equ 0x00500098

; Oracle / controller.
ORACLE             equ 0x005000A0
STRATEGY           equ 0x005000A8
CONTROL_DA         equ 0x005000B0
CONTROL_DB         equ 0x005000B8
CONTROL_COST       equ 0x005000C0

; System state.
TRINARY            equ 0x005000C8
YIN                equ 0x005000D0
PHASE              equ 0x005000D8
DEPTH              equ 0x005000E0

; Diagnostics.
FAULT              equ 0x005000E8
CONTROL_ACCEPTED   equ 0x005000F0
CONTROL_REJECTED   equ 0x005000F8


; =============================================================================
; ORACLE BITS
; =============================================================================

ORACLE_WATER_BROKEN    equ 0x01
ORACLE_EARTH_PATTERN   equ 0x02
ORACLE_EARTH_MAGNITUDE equ 0x04
ORACLE_WIND_FIXED      equ 0x08
ORACLE_WIND_DIVERGE    equ 0x10
ORACLE_CONTROLLER_MOVE equ 0x20
ORACLE_CRITICAL        equ 0x80


; =============================================================================
; STRATEGIES
; =============================================================================

STRATEGY_FLOWING       equ 0
STRATEGY_DAMPING       equ 1
STRATEGY_NONACTION     equ 2
STRATEGY_CONVERGE      equ 3
STRATEGY_CRITICAL      equ 7


; =============================================================================
; BOOT
; =============================================================================

boot_start:

    cli

    xor ax, ax
    mov ds, ax
    mov es, ax
    mov ss, ax
    mov sp, 0x7C00

    mov [boot_drive], dl


    ; -------------------------------------------------------------------------
    ; Text mode.
    ; -------------------------------------------------------------------------

    mov ax, 0x0003
    int 0x10


    ; -------------------------------------------------------------------------
    ; Load payload with INT13 extensions.
    ; -------------------------------------------------------------------------

    mov ah, 0x41
    mov bx, 0x55AA
    mov dl, [boot_drive]
    int 0x13

    jc boot_disk_error

    cmp bx, 0xAA55
    jne boot_disk_error

    test cl, 1
    jz boot_disk_error


    mov si, disk_address_packet
    mov dl, [boot_drive]
    mov ah, 0x42
    int 0x13

    jc boot_disk_error


    ; -------------------------------------------------------------------------
    ; A20.
    ; -------------------------------------------------------------------------

    mov ax, 0x2401
    int 0x15

    in al, 0x92
    or al, 2
    and al, 0xFE
    out 0x92, al


    ; -------------------------------------------------------------------------
    ; GDT.
    ; -------------------------------------------------------------------------

    lgdt [gdt_ptr]


    ; -------------------------------------------------------------------------
    ; Protected mode.
    ; -------------------------------------------------------------------------

    mov eax, cr0
    or eax, 1
    mov cr0, eax

    jmp dword 0x08:protected_entry


; =============================================================================
; BOOT ERROR
; =============================================================================

boot_disk_error:

    mov si, boot_error_msg

.boot_print:

    lodsb

    test al, al
    jz .halt

    mov ah, 0x0E
    xor bh, bh
    int 0x10

    jmp .boot_print


.halt:

    cli
    hlt
    jmp .halt


boot_drive:
    db 0

boot_error_msg:
    db "HDGL DISK ERROR",0


; =============================================================================
; DISK ADDRESS PACKET
; =============================================================================

disk_address_packet:

    db 0x10
    db 0

    dw PAYLOAD_SECTORS

    dw 0

    dw LOAD_SEG

    dq 1


; =============================================================================
; GDT
; =============================================================================

align 8

gdt_base:

    dq 0x0000000000000000
    dq 0x00CF9A000000FFFF
    dq 0x00CF92000000FFFF
    dq 0x00AF9A000000FFFF

gdt_end:


gdt_ptr:

    dw gdt_end - gdt_base - 1
    dd gdt_base


; =============================================================================
; BOOT SECTOR
; =============================================================================

times 510 - ($ - $$) db 0
dw 0xAA55


; =============================================================================
; 32-BIT PROTECTED MODE
; =============================================================================

BITS 32

protected_entry:

    cli

    mov ax, 0x10

    mov ds, ax
    mov es, ax
    mov ss, ax

    mov esp, BSP_STACK


    call build_page_tables


    ; Enable PAE.
    mov eax, cr4
    or eax, (1 << 5)
    mov cr4, eax


    ; Enable long mode.
    mov ecx, 0xC0000080
    rdmsr

    or eax, (1 << 8)

    wrmsr


    ; CR3.
    mov eax, PAGE_PML4
    mov cr3, eax


    ; Enable paging.
    mov eax, cr0
    or eax, (1 << 31)
    mov cr0, eax


    jmp dword 0x18:long_mode_entry


; =============================================================================
; PAGE TABLES
; =============================================================================

build_page_tables:

    pushad

    mov edi, PAGE_PML4

    xor eax, eax

    mov ecx, 0x6000 / 4

    rep stosd


    ; PML4[0] -> PDPT.
    mov dword [PAGE_PML4 + 0], PAGE_PDPT | 0x003
    mov dword [PAGE_PML4 + 4], 0


    ; PDPT.
    mov dword [PAGE_PDPT + 0], PAGE_PD0 | 0x003
    mov dword [PAGE_PDPT + 8], PAGE_PD1 | 0x003
    mov dword [PAGE_PDPT + 16], PAGE_PD2 | 0x003
    mov dword [PAGE_PDPT + 24], PAGE_PD3 | 0x003


    ; PD0 = 0 .. 1 GiB.
    mov edi, PAGE_PD0
    xor eax, eax

    mov ecx, 512

.pd0:

    mov edx, eax
    or edx, 0x83

    mov [edi], edx
    mov dword [edi + 4], 0

    add eax, 0x200000
    add edi, 8

    loop .pd0


    ; PD1 = 1 .. 2 GiB.
    mov edi, PAGE_PD1
    mov eax, 0x40000000

    mov ecx, 512

.pd1:

    mov edx, eax
    or edx, 0x83

    mov [edi], edx
    mov dword [edi + 4], 0

    add eax, 0x200000
    add edi, 8

    loop .pd1


    ; PD2 = 2 .. 3 GiB.
    mov edi, PAGE_PD2
    mov eax, 0x80000000

    mov ecx, 512

.pd2:

    mov edx, eax
    or edx, 0x83

    mov [edi], edx
    mov dword [edi + 4], 0

    add eax, 0x200000
    add edi, 8

    loop .pd2


    ; PD3 = 3 .. 4 GiB.
    mov edi, PAGE_PD3
    mov eax, 0xC0000000

    mov ecx, 512

.pd3:

    mov edx, eax
    or edx, 0x83

    mov [edi], edx
    mov dword [edi + 4], 0

    add eax, 0x200000
    add edi, 8

    loop .pd3


    popad
    ret


; =============================================================================
; 64-BIT MODE
; =============================================================================

BITS 64

long_mode_entry:

    cli

    mov ax, 0x10

    mov ds, ax
    mov es, ax
    mov ss, ax

    mov rsp, BSP_STACK


    ; -------------------------------------------------------------------------
    ; Initialize canonical state.
    ;
    ; X0 = 0φ + 1.
    ; -------------------------------------------------------------------------

    mov qword [STATE_A], 0
    mov qword [STATE_B], 1
    mov qword [STATE_K], 0


    ; -------------------------------------------------------------------------
    ; Clear controller state.
    ; -------------------------------------------------------------------------

    mov qword [CONTROL_A], 0
    mov qword [CONTROL_B], 1

    mov qword [FIRE_A], 0
    mov qword [FIRE_B], 1

    mov qword [WATER_A], 0
    mov qword [WATER_B], 1
    mov qword [WATER_OK], 0


    mov qword [EARTH_N], 1
    mov qword [EARTH_N_FIRE], 1
    mov qword [EARTH_DELTA], 0
    mov qword [EARTH_COST], 0


    mov qword [WIND_RES_A], 0
    mov qword [WIND_RES_B], -1
    mov qword [WIND_COST], 1
    mov qword [WIND_FIXED], 0


    mov qword [ORACLE], 0
    mov qword [STRATEGY], STRATEGY_FLOWING

    mov qword [CONTROL_DA], 0
    mov qword [CONTROL_DB], 0
    mov qword [CONTROL_COST], 0

    mov qword [TRINARY], 1

    mov qword [YIN], 2

    mov qword [PHASE], 0
    mov qword [DEPTH], 0

    mov qword [FAULT], 0
    mov qword [CONTROL_ACCEPTED], 0
    mov qword [CONTROL_REJECTED], 0


    ; -------------------------------------------------------------------------
    ; VGA.
    ; -------------------------------------------------------------------------

    call vga_init


    ; -------------------------------------------------------------------------
    ; Main cybernetic loop.
    ; -------------------------------------------------------------------------

cybernetic_cycle:


    ; -------------------------------------------------------------------------
    ; Clear current-cycle oracle.
    ; -------------------------------------------------------------------------

    mov qword [ORACLE], 0


    ; -------------------------------------------------------------------------
    ; OBSERVE CURRENT STATE.
    ; -------------------------------------------------------------------------

    call earth_current
    call wind_current


    ; -------------------------------------------------------------------------
    ; CONTROLLER.
    ;
    ; Chooses among the local 3x3 neighborhood.
    ; -------------------------------------------------------------------------

    call controller_select


    ; -------------------------------------------------------------------------
    ; ACTUATE.
    ;
    ; FIRE(controlled input) -> predicted next state.
    ; -------------------------------------------------------------------------

    call fire_controlled


    ; -------------------------------------------------------------------------
    ; WATER verifies the forward operator exactly.
    ; -------------------------------------------------------------------------

    call water_verify


    test rax, rax
    jnz .water_ok


    ; Controller produced an invalid transition.
    ; Reject it and retain the prior state.

    inc qword [CONTROL_REJECTED]

    or qword [ORACLE], ORACLE_WATER_BROKEN

    mov qword [STRATEGY], STRATEGY_NONACTION

    mov qword [WATER_OK], 0

    jmp .post_control


.water_ok:

    mov qword [WATER_OK], 1


    ; -------------------------------------------------------------------------
    ; EARTH verifies predicted-state invariant.
    ; -------------------------------------------------------------------------

    call earth_predicted


    ; -------------------------------------------------------------------------
    ; WIND verifies predicted-state fixed-point residual.
    ; -------------------------------------------------------------------------

    call wind_predicted


    ; -------------------------------------------------------------------------
    ; Strategy.
    ; -------------------------------------------------------------------------

    call strategy_select


    ; -------------------------------------------------------------------------
    ; COMMIT:
    ;
    ; The controller has already modified the state trajectory.
    ; The FIRE result is now the actual new state.
    ; -------------------------------------------------------------------------

    mov rax, [FIRE_A]
    mov rbx, [FIRE_B]

    mov [STATE_A], rax
    mov [STATE_B], rbx


    inc qword [CONTROL_ACCEPTED]


    ; -------------------------------------------------------------------------
    ; Cycle bookkeeping.
    ; -------------------------------------------------------------------------

    inc qword [STATE_K]
    inc qword [DEPTH]

    inc qword [PHASE]

    and qword [PHASE], 3


    ; YIN:
    ;
    ;     s -> s² - 2
    ;
    mov rax, [YIN]
    imul rax, rax
    sub rax, 2
    mov [YIN], rax


.post_control:


    ; -------------------------------------------------------------------------
    ; Display periodically.
    ; -------------------------------------------------------------------------

    mov rax, [STATE_K]
    test rax, PRINT_MASK
    jnz cybernetic_cycle

    call vga_update

    jmp cybernetic_cycle


; =============================================================================
; CONTROLLER
; =============================================================================
;
; One-step model predictive controller.
;
; The controller evaluates the 3x3 neighborhood:
;
;     da ∈ {-1,0,+1}
;     db ∈ {-1,0,+1}
;
; Candidate:
;
;     C = (a+da,b+db)
;
; FIRE:
;
;     F(C) = (C_a+C_b,C_a)
;
; Cost:
;
;     WIND_COST(F(C))
;       +
;     EARTH_COST(F(C))
;
; The candidate with the minimum cost becomes the actual actuator input.
;
; This is the point where the architecture stops being a passive oracle.
;
; =============================================================================

controller_select:

    ; -------------------------------------------------------------------------
    ; Current state.
    ; -------------------------------------------------------------------------

    mov r8, [STATE_A]
    mov r9, [STATE_B]


    ; -------------------------------------------------------------------------
    ; Current best cost = max.
    ; -------------------------------------------------------------------------

    mov rax, 0xFFFFFFFFFFFFFFFF

    mov [CONTROL_COST], rax


    ; Best correction initially zero.
    mov qword [CONTROL_DA], 0
    mov qword [CONTROL_DB], 0


    ; -------------------------------------------------------------------------
    ; da=-1 db=-1
    ; -------------------------------------------------------------------------

    mov r10, -1
    mov r11, -1

    call controller_candidate

    ; -------------------------------------------------------------------------
    ; da=-1 db=0
    ; -------------------------------------------------------------------------

    mov r10, -1
    xor r11d, r11d

    call controller_candidate

    ; -------------------------------------------------------------------------
    ; da=-1 db=+1
    ; -------------------------------------------------------------------------

    mov r10, -1
    mov r11, 1

    call controller_candidate

    ; -------------------------------------------------------------------------
    ; da=0 db=-1
    ; -------------------------------------------------------------------------

    xor r10d, r10d
    mov r11, -1

    call controller_candidate

    ; -------------------------------------------------------------------------
    ; da=0 db=0
    ; -------------------------------------------------------------------------

    xor r10d, r10d
    xor r11d, r11d

    call controller_candidate

    ; -------------------------------------------------------------------------
    ; da=0 db=+1
    ; -------------------------------------------------------------------------

    xor r10d, r10d
    mov r11, 1

    call controller_candidate

    ; -------------------------------------------------------------------------
    ; da=+1 db=-1
    ; -------------------------------------------------------------------------

    mov r10, 1
    mov r11, -1

    call controller_candidate

    ; -------------------------------------------------------------------------
    ; da=+1 db=0
    ; -------------------------------------------------------------------------

    mov r10, 1
    xor r11d, r11d

    call controller_candidate

    ; -------------------------------------------------------------------------
    ; da=+1 db=+1
    ; -------------------------------------------------------------------------

    mov r10, 1
    mov r11, 1

    call controller_candidate


    ; -------------------------------------------------------------------------
    ; If any non-zero correction was selected, expose oracle bit.
    ; -------------------------------------------------------------------------

    mov rax, [CONTROL_DA]
    or rax, [CONTROL_DB]

    jz .no_move

    or qword [ORACLE], ORACLE_CONTROLLER_MOVE

.no_move:

    ret


; =============================================================================
; CONTROLLER CANDIDATE
; =============================================================================
;
; INPUT:
;
;     r8  = current a
;     r9  = current b
;     r10 = da
;     r11 = db
;
; Destroys rax-r15.
;
; =============================================================================

controller_candidate:

    push r8
    push r9
    push r10
    push r11


    ; Candidate input.
    lea r12, [r8 + r10]
    lea r13, [r9 + r11]


    ; Candidate FIRE:
    ;
    ;     next_a = ca + cb
    ;     next_b = ca
    ;

    mov r14, r12
    add r14, r13

    mov r15, r12


    ; -------------------------------------------------------------------------
    ; Candidate WATER consistency is structurally guaranteed because FIRE was
    ; applied to the candidate itself.
    ;
    ; Still perform the inverse explicitly.
    ; -------------------------------------------------------------------------

    mov rax, r14
    mov rbx, r15

    mov rcx, r15
    mov rdx, r14
    sub rdx, r15

    cmp rcx, r12
    jne .candidate_done

    cmp rdx, r13
    jne .candidate_done


    ; -------------------------------------------------------------------------
    ; WIND predicted residual.
    ; -------------------------------------------------------------------------

    mov rdi, r14
    mov rsi, r15

    call wind_cost_pair

    mov rbx, rax


    ; -------------------------------------------------------------------------
    ; EARTH predicted error.
    ;
    ; Desired Fibonacci invariant:
    ;
    ;     |N| = 1
    ;
    ; Cost = abs(|N|-1).
    ; -------------------------------------------------------------------------

    mov rdi, r14
    mov rsi, r15

    call earth_cost_pair

    add rbx, rax


    ; -------------------------------------------------------------------------
    ; Controller inertia:
    ;
    ; Prefer zero correction when costs tie.
    ; -------------------------------------------------------------------------

    mov rax, [CONTROL_COST]

    cmp rbx, rax
    jae .candidate_done


    mov [CONTROL_COST], rbx

    pop r11
    pop r10
    pop r9
    pop r8

    ; Original candidate correction values survive the pop.
    mov [CONTROL_DA], r10
    mov [CONTROL_DB], r11

    ret


.candidate_done:

    pop r11
    pop r10
    pop r9
    pop r8

    ret


; =============================================================================
; FIRE — ACTUATOR
; =============================================================================
;
; FIRE receives CONTROL_A/B by applying the selected correction to STATE_A/B.
;
; Then:
;
;     F(a,b) = (a+b,a)
;
; This is the actual plant transition.
;
; =============================================================================

fire_controlled:

    mov r8, [STATE_A]
    mov r9, [STATE_B]

    mov r10, [CONTROL_DA]
    mov r11, [CONTROL_DB]

    add r8, r10
    add r9, r11

    mov [CONTROL_A], r8
    mov [CONTROL_B], r9


    mov rax, r8
    add rax, r9

    mov [FIRE_A], rax
    mov [FIRE_B], r8

    ret


; =============================================================================
; WATER — INVERSE VERIFIER
; =============================================================================

water_verify:

    mov rax, [FIRE_A]
    mov rbx, [FIRE_B]

    ; W(FIRE):
    ;
    ;     water_a = FIRE_B
    ;     water_b = FIRE_A - FIRE_B
    ;

    mov rcx, rbx

    mov rdx, rax
    sub rdx, rbx

    mov [WATER_A], rcx
    mov [WATER_B], rdx


    cmp rcx, [CONTROL_A]
    jne .broken

    cmp rdx, [CONTROL_B]
    jne .broken


    and qword [ORACLE], ~ORACLE_WATER_BROKEN

    mov rax, 1

    ret


.broken:

    or qword [ORACLE], ORACLE_WATER_BROKEN
    or qword [ORACLE], ORACLE_CRITICAL

    mov rax, 0

    ret


; =============================================================================
; EARTH CURRENT
; =============================================================================
;
; Nφ(a,b) = -a² + ab + b²
;
; =============================================================================

earth_current:

    mov r8, [STATE_A]
    mov r9, [STATE_B]

    call earth_pair

    mov [EARTH_N], rax

    ; Trinary projection.
    test rax, rax

    jz .zero

    js .negative

    mov qword [TRINARY], 1

    ret


.negative:

    mov qword [TRINARY], -1

    ret


.zero:

    mov qword [TRINARY], 0

    ret


; =============================================================================
; EARTH PREDICTED
; =============================================================================

earth_predicted:

    mov rdi, [FIRE_A]
    mov rsi, [FIRE_B]

    call earth_pair

    mov [EARTH_N_FIRE], rax


    mov rcx, [EARTH_N]
    mov rdx, rax

    sub rdx, rcx

    mov [EARTH_DELTA], rdx


    ; Cost = abs(|N|-1)
    mov rdi, rax

    call abs_qword

    cmp rax, 1

    ja .too_large

    jb .too_small

    ; exactly ±1.
    and qword [ORACLE], ~(
        ORACLE_EARTH_PATTERN |
        ORACLE_EARTH_MAGNITUDE
    )

    mov qword [EARTH_COST], 0

    ret


.too_large:

    sub rax, 1

    mov [EARTH_COST], rax

    or qword [ORACLE], ORACLE_EARTH_MAGNITUDE

    ret


.too_small:

    mov rbx, 1
    sub rbx, rax

    mov [EARTH_COST], rbx

    or qword [ORACLE], ORACLE_EARTH_MAGNITUDE

    ret


; =============================================================================
; EARTH PAIR
;
; INPUT:
;     rdi = a
;     rsi = b
;
; OUTPUT:
;     rax = -a² + ab + b²
; =============================================================================

earth_pair:

    mov rax, rdi
    imul rax, rdi
    neg rax

    mov rbx, rdi
    imul rbx, rsi

    add rax, rbx

    mov rbx, rsi
    imul rbx, rsi

    add rax, rbx

    ret


; =============================================================================
; WIND CURRENT
; =============================================================================
;
; Fixed-point residual:
;
;     Rφ = a² + 2ab - a
;     Rc = a² + b² - b - 1
;
; =============================================================================

wind_current:

    mov rdi, [STATE_A]
    mov rsi, [STATE_B]

    call wind_pair

    mov [WIND_RES_A], rax
    mov [WIND_RES_B], rbx


    ; Cost = |Rφ| + |Rc|.
    mov rdi, rax
    call abs_qword
    mov rcx, rax

    mov rdi, rbx
    call abs_qword
    add rax, rcx

    mov [WIND_COST], rax


    test rax, rax
    jnz .not_fixed

    mov qword [WIND_FIXED], 1
    or qword [ORACLE], ORACLE_WIND_FIXED

    ret


.not_fixed:

    mov qword [WIND_FIXED], 0

    and qword [ORACLE], ~ORACLE_WIND_FIXED

    ret


; =============================================================================
; WIND PREDICTED
; =============================================================================

wind_predicted:

    mov rdi, [FIRE_A]
    mov rsi, [FIRE_B]

    call wind_pair

    mov [WIND_RES_A], rax
    mov [WIND_RES_B], rbx


    mov rdi, rax
    call abs_qword
    mov rcx, rax

    mov rdi, rbx
    call abs_qword

    add rax, rcx

    mov [WIND_COST], rax


    test rax, rax
    jnz .not_fixed

    mov qword [WIND_FIXED], 1

    or qword [ORACLE], ORACLE_WIND_FIXED

    ret


.not_fixed:

    mov qword [WIND_FIXED], 0

    and qword [ORACLE], ~ORACLE_WIND_FIXED

    ret


; =============================================================================
; WIND PAIR
;
; INPUT:
;     rdi = a
;     rsi = b
;
; OUTPUT:
;     rax = phi coefficient residual
;     rbx = constant residual
; =============================================================================

wind_pair:

    ; -------------------------------------------------------------------------
    ; Rφ = a² + 2ab - a
    ; -------------------------------------------------------------------------

    mov rax, rdi
    imul rax, rdi

    mov rcx, rdi
    imul rcx, rsi

    add rcx, rcx

    add rax, rcx

    sub rax, rdi


    ; -------------------------------------------------------------------------
    ; Rc = a² + b² - b - 1
    ; -------------------------------------------------------------------------

    mov rbx, rdi
    imul rbx, rdi

    mov rcx, rsi
    imul rcx, rsi

    add rbx, rcx

    sub rbx, rsi

    dec rbx

    ret


; =============================================================================
; WIND COST
;
; INPUT:
;     rdi = a
;     rsi = b
;
; OUTPUT:
;     rax = |Rφ| + |Rc|
; =============================================================================

wind_cost_pair:

    call wind_pair

    mov r8, rax
    mov r9, rbx

    mov rdi, r8
    call abs_qword

    mov r8, rax

    mov rdi, r9
    call abs_qword

    add rax, r8

    ret


; =============================================================================
; EARTH COST
;
; INPUT:
;     rdi = a
;     rsi = b
;
; OUTPUT:
;     rax = abs(abs(N)-1)
; =============================================================================

earth_cost_pair:

    call earth_pair

    mov r8, rax

    mov rdi, r8
    call abs_qword

    cmp rax, 1

    ja .large

    cmp rax, 1

    je .zero

    ; |N| = 0
    mov rax, 1
    ret


.large:

    dec rax
    ret


.zero:

    xor eax, eax
    ret


; =============================================================================
; STRATEGY SELECTOR
; =============================================================================

strategy_select:

    mov rax, [ORACLE]


    ; Critical.
    test al, ORACLE_CRITICAL
    jnz .critical


    ; Water failure.
    test al, ORACLE_WATER_BROKEN
    jnz .nonaction


    ; Wind fixed point.
    test al, ORACLE_WIND_FIXED
    jnz .converge


    ; Controller moved state.
    test al, ORACLE_CONTROLLER_MOVE
    jnz .damping


    ; Normal.
    mov qword [STRATEGY], STRATEGY_FLOWING

    ret


.damping:

    mov qword [STRATEGY], STRATEGY_DAMPING

    ret


.nonaction:

    mov qword [STRATEGY], STRATEGY_NONACTION

    ; If verification fails, reject the transition.
    mov qword [FAULT], 1

    ret


.converge:

    mov qword [STRATEGY], STRATEGY_CONVERGE

    ret


.critical:

    mov qword [STRATEGY], STRATEGY_CRITICAL
    mov qword [FAULT], 1

    ret


; =============================================================================
; ABS
; =============================================================================

abs_qword:

    test rdi, rdi

    jns .positive

    neg rdi

.positive:

    mov rax, rdi

    ret


; =============================================================================
; VGA INITIALIZATION
; =============================================================================

vga_init:

    mov rdi, VGA_BASE

    xor eax, eax

    mov rcx, (80 * 25 * 2) / 8

    rep stosq


    ; Header.
    mov rdi, VGA_BASE

    mov rsi, str_title

    mov bl, 0x0F

    call vga_string

    ret


; =============================================================================
; VGA UPDATE
; =============================================================================

vga_update:

    ; -------------------------------------------------------------------------
    ; Clear rows 1..24.
    ; -------------------------------------------------------------------------

    mov rdi, VGA_BASE + 160

    xor eax, eax

    mov rcx, (160 * 24) / 8

    rep stosq


    ; -------------------------------------------------------------------------
    ; Row 0 title.
    ; -------------------------------------------------------------------------

    mov rdi, VGA_BASE

    mov rsi, str_title

    mov bl, 0x0F

    call vga_string


    ; -------------------------------------------------------------------------
    ; Row 2 state.
    ; -------------------------------------------------------------------------

    mov rdi, VGA_BASE + (2 * 160)

    mov rsi, str_state

    call vga_string

    mov rax, [STATE_K]

    mov rdi, VGA_BASE + (2 * 160) + 10*2

    call vga_hex_qword


    mov rax, [STATE_A]

    mov rdi, VGA_BASE + (2 * 160) + 30*2

    call vga_hex_qword


    mov rax, [STATE_B]

    mov rdi, VGA_BASE + (2 * 160) + 50*2

    call vga_hex_qword


    ; -------------------------------------------------------------------------
    ; Row 4 controller.
    ; -------------------------------------------------------------------------

    mov rdi, VGA_BASE + (4 * 160)

    mov rsi, str_control

    call vga_string


    mov rax, [CONTROL_DA]

    mov rdi, VGA_BASE + (4 * 160) + 12*2

    call vga_hex_qword


    mov rax, [CONTROL_DB]

    mov rdi, VGA_BASE + (4 * 160) + 32*2

    call vga_hex_qword


    mov rax, [CONTROL_COST]

    mov rdi, VGA_BASE + (4 * 160) + 52*2

    call vga_hex_qword


    ; -------------------------------------------------------------------------
    ; Row 6 FIRE.
    ; -------------------------------------------------------------------------

    mov rdi, VGA_BASE + (6 * 160)

    mov rsi, str_fire

    call vga_string


    mov rax, [FIRE_A]

    mov rdi, VGA_BASE + (6 * 160) + 12*2

    call vga_hex_qword


    mov rax, [FIRE_B]

    mov rdi, VGA_BASE + (6 * 160) + 32*2

    call vga_hex_qword


    ; -------------------------------------------------------------------------
    ; Row 8 WATER.
    ; -------------------------------------------------------------------------

    mov rdi, VGA_BASE + (8 * 160)

    mov rsi, str_water

    call vga_string


    mov rax, [WATER_A]

    mov rdi, VGA_BASE + (8 * 160) + 12*2

    call vga_hex_qword


    mov rax, [WATER_B]

    mov rdi, VGA_BASE + (8 * 160) + 32*2

    call vga_hex_qword


    mov rax, [WATER_OK]

    mov rdi, VGA_BASE + (8 * 160) + 52*2

    call vga_hex_qword


    ; -------------------------------------------------------------------------
    ; Row 10 EARTH.
    ; -------------------------------------------------------------------------

    mov rdi, VGA_BASE + (10 * 160)

    mov rsi, str_earth

    call vga_string


    mov rax, [EARTH_N]

    mov rdi, VGA_BASE + (10 * 160) + 12*2

    call vga_hex_qword


    mov rax, [EARTH_N_FIRE]

    mov rdi, VGA_BASE + (10 * 160) + 32*2

    call vga_hex_qword


    mov rax, [EARTH_DELTA]

    mov rdi, VGA_BASE + (10 * 160) + 52*2

    call vga_hex_qword


    ; -------------------------------------------------------------------------
    ; Row 12 WIND.
    ; -------------------------------------------------------------------------

    mov rdi, VGA_BASE + (12 * 160)

    mov rsi, str_wind

    call vga_string


    mov rax, [WIND_RES_A]

    mov rdi, VGA_BASE + (12 * 160) + 12*2

    call vga_hex_qword


    mov rax, [WIND_RES_B]

    mov rdi, VGA_BASE + (12 * 160) + 32*2

    call vga_hex_qword


    mov rax, [WIND_COST]

    mov rdi, VGA_BASE + (12 * 160) + 52*2

    call vga_hex_qword


    ; -------------------------------------------------------------------------
    ; Row 14 Oracle / strategy.
    ; -------------------------------------------------------------------------

    mov rdi, VGA_BASE + (14 * 160)

    mov rsi, str_oracle

    call vga_string


    mov rax, [ORACLE]

    mov rdi, VGA_BASE + (14 * 160) + 8*2

    call vga_hex_qword


    mov rax, [STRATEGY]

    mov rdi, VGA_BASE + (14 * 160) + 32*2

    call vga_hex_qword


    ; -------------------------------------------------------------------------
    ; Row 16 YIN / phase / depth.
    ; -------------------------------------------------------------------------

    mov rdi, VGA_BASE + (16 * 160)

    mov rsi, str_yin

    call vga_string


    mov rax, [YIN]

    mov rdi, VGA_BASE + (16 * 160) + 8*2

    call vga_hex_qword


    mov rax, [PHASE]

    mov rdi, VGA_BASE + (16 * 160) + 28*2

    call vga_hex_qword


    mov rax, [DEPTH]

    mov rdi, VGA_BASE + (16 * 160) + 48*2

    call vga_hex_qword


    ; -------------------------------------------------------------------------
    ; Row 18 controller acceptance/rejection.
    ; -------------------------------------------------------------------------

    mov rdi, VGA_BASE + (18 * 160)

    mov rsi, str_stats

    call vga_string


    mov rax, [CONTROL_ACCEPTED]

    mov rdi, VGA_BASE + (18 * 160) + 10*2

    call vga_hex_qword


    mov rax, [CONTROL_REJECTED]

    mov rdi, VGA_BASE + (18 * 160) + 32*2

    call vga_hex_qword


    ; -------------------------------------------------------------------------
    ; Row 20 trinary.
    ; -------------------------------------------------------------------------

    mov rdi, VGA_BASE + (20 * 160)

    mov rsi, str_trinary

    call vga_string


    mov rax, [TRINARY]

    mov rdi, VGA_BASE + (20 * 160) + 10*2

    call vga_hex_qword


    ; -------------------------------------------------------------------------
    ; Row 22 fault.
    ; -------------------------------------------------------------------------

    mov rdi, VGA_BASE + (22 * 160)

    mov rsi, str_fault

    call vga_string


    mov rax, [FAULT]

    mov rdi, VGA_BASE + (22 * 160) + 10*2

    call vga_hex_qword


    ret


; =============================================================================
; VGA STRING
; =============================================================================
;
; INPUT:
;     rdi = destination
;     rsi = zero-terminated string
;     bl  = attribute
;
; =============================================================================

vga_string:

.next:

    lodsb

    test al, al

    jz .done

    mov [rdi], al
    mov [rdi + 1], bl

    add rdi, 2

    jmp .next


.done:

    ret


; =============================================================================
; VGA HEX QWORD
; =============================================================================

vga_hex_qword:

    push rax
    push rbx
    push rcx
    push rdx
    push rsi
    push rdi

    mov rbx, rdi

    mov rcx, 16


.loop:

    mov rdx, rax

    shr rdx, 60

    and edx, 0x0F

    mov dl, [hex_digits + rdx]

    mov [rbx], dl

    mov byte [rbx + 1], 0x07

    add rbx, 2

    shl rax, 4

    loop .loop


    pop rdi
    pop rsi
    pop rdx
    pop rcx
    pop rbx
    pop rax

    ret


; =============================================================================
; STRINGS
; =============================================================================

str_title:
    db "HDGL REAL CYBERNETIC CORE  OBSERVE-CONTROL-ACT-VERIFY",0


str_state:
    db "STATE K=          A=                  B=",0


str_control:
    db "CONTROL DA=                  DB=                  COST=",0


str_fire:
    db "FIRE   A=                  B=",0


str_water:
    db "WATER  A=                  B=                  OK=",0


str_earth:
    db "EARTH  N=                  NF=                 DELTA=",0


str_wind:
    db "WIND   RA=                 RB=                 COST=",0


str_oracle:
    db "ORACLE=                  STRATEGY=",0


str_yin:
    db "YIN    S=                  PHASE=              DEPTH=",0


str_stats:
    db "CONTROL ACCEPTED=        REJECTED=",0


str_trinary:
    db "TRINARY=",0


str_fault:
    db "FAULT=",0


hex_digits:
    db "0123456789ABCDEF"


; =============================================================================
; END
; =============================================================================

analog-cybernetic0.zip (12.5 KB)

II_analog_boot.zip (376.3 KB)