Files
AR-Autopilot/arautopilot/core/adaptive_tuner.py
T
alro65 a2f3e82f17 sprint-9: integration tests + hardening + operator manual
Integration tests (64 new tests, 462 total):
- test_integration_cascade: full cascade closed-loop simulation --
  outer PID → inner PID → rudder dynamics → vessel heading; verifies
  convergence across small/90°/180° turns, wrap-around, and low speed
- test_integration_ekf_pid: EKF-smoothed heading feeding outer PID;
  confirms EKF reduces rudder total-variation vs raw noisy heading
- test_integration_alarm_audit: alarm engine → audit log hash-chain;
  verify, tamper detection, cross-session reload, multi-alarm logging
- test_modbus_utils: 38 tests for scale/raw conversion, bounds checking,
  heading/rudder helpers, signed int16 two's-complement round-trip

Hardening:
- heading_ekf: guard NaN/inf in update_heading() and update_rot() -- skip
  bad measurements silently rather than corrupting filter state
- adaptive_tuner: guard NaN/inf in step() -- ignore corrupt error samples
- modbus_utils.py: new shared module with scale_to_raw, scale_to_raw_signed,
  raw_signed_to_scaled, clamp_uint16, validate_holding_write,
  heading_deg_to_raw, rudder_deg_to_raw_signed

Documentation:
- docs/operator_manual.md: 15-section operator manual covering safety,
  installation, all operating modes, alarm reference, commissioning,
  fault-finding, Modbus register summary, and activation/audit log procedure

Co-Authored-By: Claude Sonnet 4.6 <noreply@anthropic.com>
2026-05-20 03:35:23 -04:00

144 lines
4.9 KiB
Python

"""Adaptive gain tuner -- Sprint 8.
Watches the steady-state heading error and adjusts the outer-loop Kp/Ki
within the bounds defined by ``PidConfig.adaptive_max_deviation_pct``.
The strategy is a simple integral-error gradient scheme:
- If |mean_error| > dead_band for a sustained window, nudge Kp up by step_pct.
- If the response is oscillating (error sign changes frequently), nudge Kp down.
- Ki is adjusted proportionally to maintain the ZN ratio Ki = 2*Kp / Tu_est.
- Kd is not adapted (derivative magnifies noise; ZN auto-tune sets it once).
All changes are bounded to ±adaptive_max_deviation_pct of the base gains
(brief section 6: "never outside ±50 %").
Usage::
tuner = AdaptiveTuner(pid_config, base_gains)
# On each outer-loop tick (10 Hz):
new_gains = tuner.step(heading_error_deg, dt_s=0.1)
if new_gains is not None:
apply_outer_gains(new_gains)
"""
from __future__ import annotations
import math
from dataclasses import dataclass, field
from arautopilot.core.pid_config import PidConfig, PidGains
@dataclass
class AdaptiveTuner:
"""Gradient-descent adaptive gain tuner for the outer PID loop.
Parameters
----------
config:
PidConfig that owns the base gains and adaptive bounds.
base_gains:
The current base gains (set by commissioning or default).
dead_band_deg:
Error below which no adaptation occurs.
window_steps:
Number of 10 Hz steps over which the error statistics are computed.
step_pct:
Fractional Kp adjustment per adaptation event (default 2 %).
"""
config: PidConfig
base_gains: PidGains
dead_band_deg: float = 1.0
window_steps: int = 100 # 10 seconds
step_pct: float = 0.02 # 2 % per step
_error_buffer: list[float] = field(default_factory=list)
_current_kp: float = field(init=False)
_current_ki: float = field(init=False)
_current_kd: float = field(init=False)
def __post_init__(self) -> None:
self._current_kp = self.base_gains.kp
self._current_ki = self.base_gains.ki
self._current_kd = self.base_gains.kd
# ------------------------------------------------------------------
@property
def current_gains(self) -> PidGains:
return PidGains(kp=self._current_kp, ki=self._current_ki, kd=self._current_kd)
def step(self, error_deg: float, dt_s: float = 0.1) -> PidGains | None:
"""Feed one heading error sample; return updated gains if adapted.
Returns ``None`` if no adaptation occurred this step.
"""
if not self.config.adaptive_enabled:
return None
if not math.isfinite(error_deg):
return None
self._error_buffer.append(error_deg)
if len(self._error_buffer) > self.window_steps:
self._error_buffer.pop(0)
if len(self._error_buffer) < self.window_steps:
return None # buffer not yet full
mean_abs = sum(abs(e) for e in self._error_buffer) / len(self._error_buffer)
# Count sign changes (oscillation indicator)
sign_changes = sum(
1 for i in range(1, len(self._error_buffer))
if (self._error_buffer[i] >= 0) != (self._error_buffer[i - 1] >= 0)
)
oscillating = sign_changes > self.window_steps * 0.3 # > 30 % sign flips
# Decision
if oscillating:
# Reduce Kp to damp oscillation.
return self._adjust_kp(-self.step_pct)
elif mean_abs > self.dead_band_deg:
# Increase Kp to reduce steady-state error.
return self._adjust_kp(+self.step_pct)
return None
def _adjust_kp(self, delta_frac: float) -> PidGains | None:
"""Adjust Kp by ``delta_frac`` fraction (signed), clamped to bounds."""
new_kp = self._current_kp * (1.0 + delta_frac)
# Clamp to ±adaptive_max_deviation_pct of base.
limit = self.config.adaptive_max_deviation_pct / 100.0
lo = self.base_gains.kp * (1.0 - limit)
hi = self.base_gains.kp * (1.0 + limit)
new_kp = max(lo, min(hi, new_kp))
if new_kp == self._current_kp:
return None
# Adjust Ki proportionally (maintain integral-to-proportional ratio).
if self.base_gains.kp > 0:
ki_ratio = self.base_gains.ki / self.base_gains.kp
else:
ki_ratio = 0.0
new_ki = new_kp * ki_ratio
# Clamp Ki as well.
ki_lo = self.base_gains.ki * (1.0 - limit)
ki_hi = self.base_gains.ki * (1.0 + limit)
new_ki = max(ki_lo, min(ki_hi, new_ki))
self._current_kp = new_kp
self._current_ki = new_ki
# Clear buffer after each adaptation to avoid consecutive nudges.
self._error_buffer.clear()
return self.current_gains
def reset(self) -> None:
"""Reset to base gains."""
self._current_kp = self.base_gains.kp
self._current_ki = self.base_gains.ki
self._current_kd = self.base_gains.kd
self._error_buffer.clear()