sprint-1: firmware ESP32 base -- STANDBY + Modbus + NMEA 2000 + watchdog

End-to-end implementation of Sprint 1 per docs/sprint-1-plan.md.

Builds: pio run -e esp32-dev SUCCESS, RAM 6.7%, Flash 26.5% (347 KB).
Tests: pytest 110/110 green; pio test -e native deferred (needs host
       C++ compiler -- none on this Windows machine).

Firmware (firmware/ar_autopilot_v1/):

- platformio.ini: 4 envs (esp32-dev release, esp32-debug, native unity
  tests, check static analysis). NMEA2000-library@4.22, NMEA2000_esp32@
  1.0, eModbus@1.7.4 pinned.
- main.cpp: boot in STANDBY, FreeRTOS task spawn, returns to scheduler.
- system/: ar_log.h facade, task_config.h (priorities/stacks/cores
  central table), heartbeat (1 Hz LED + uptime).
- modes/: STANDBY-only state machine; non-STANDBY rejected.
- hal/: di_do.cpp (5 DI + 10 DO with debounce + last-state cache),
  rudder_sensor.cpp (100 Hz ADC + 5-sample median filter, Core 1),
  rudder_actuator.cpp (DO1/DO2/DO3 with three safety interlocks:
  power-off, STANDBY mode, limit switch).
- safety/: TWDT @ 2 s panic-on-expire; 50 Hz safety task on Core 1
  enforcing DI1 physical disengage button, DI4 external alarm,
  both-limit-switch interlock.
- protocols/modbus_slave.cpp: eModbus RTU server on UART2 @ 38400 8N1,
  slave ID 1. 17 inputs + 19 discretes + 5 holdings + 4 coils. Reads
  pull live telemetry; writes validate range and route to handlers.
- protocols/nmea2000_consumer.cpp: stack open with CAN TX=GPIO3
  RX=GPIO1, subscribed to PGN 127250 (Heading) + PGN 127251 (Rate of
  Turn). 5 s staleness flag built in for Sprint 6 alarm wiring.
- filters/median.h: templated MedianFilter<T,N> (host testable).

Cross-cutting:

- modbus_registers.yaml: single source of truth for the Modbus register
  map. 45 entries.
- tools/gen_modbus_registers.py: YAML -> C++ header + Python module
  generator with --check for drift detection.
- arautopilot/shared/modbus_register_map.py: generated Python mirror,
  imported by Studio + tools.
- arautopilot/tests/test_modbus_register_map.py: 30 tests covering
  schema, address uniqueness, range, spot-checks, and drift detection
  (fails if YAML edited without regenerating).
- firmware/ar_autopilot_v1/tools/modbus_client_test.py: manual Modbus
  client for poking the slave from a PC with USB-RS485 dongle.
- firmware/ar_autopilot_v1/test/test_median_filter/test_median.cpp:
  8 Unity tests of the median filter (host-side, no Arduino dependency).
- docs/firmware.md: full operator + integrator guide (toolchain, build,
  flash, expected boot log, troubleshooting, Sprint 1 capability matrix).

Architecture note: opted for Arduino-on-ESP32 only instead of the
proposed dual Arduino-as-ESP-IDF-component setup. Rationale documented
in CHANGELOG and docs/firmware.md -- Arduino-on-ESP32 already provides
the FreeRTOS primitives we need; dual framework adds fragility without
benefit at Sprint 1 scope. Reconsider in Sprint 8 (OTA + secure boot).

NOT in Sprint 1 (intentional per brief sec. 12):
  - PID loops (inner/outer)
  - True Course / Track Keeping
  - Full alarm catalogue beyond DI1/DI4
  - Knob driver
  - Studio GUI / dedicated display

Co-Authored-By: Claude Opus 4.7 (1M context) <noreply@anthropic.com>
This commit is contained in:
2026-05-18 10:45:56 -04:00
parent 1d7dd63327
commit 65860948b4
31 changed files with 3310 additions and 0 deletions
@@ -0,0 +1,76 @@
// =============================================================================
// median.h -- fixed-size median filter
// =============================================================================
//
// Templated median filter that holds the last N samples in a ring buffer and
// returns the median of the current window in O(N log N) (sort-copy). N is
// expected to be small (3-9), so the cost is negligible at 100 Hz.
//
// Used by:
// - hal/rudder_sensor.cpp (5-sample median to suppress ADC spikes)
//
// Host-testable: depends only on the standard library. The Unity tests in
// test/test_filters/ exercise it on the developer machine.
// =============================================================================
#pragma once
#include <algorithm>
#include <array>
#include <cstddef>
namespace arautopilot::filters {
template <typename T, std::size_t N>
class MedianFilter {
static_assert(N >= 1, "MedianFilter window must be at least 1");
static_assert(N % 2 == 1, "MedianFilter window must be odd for an unambiguous median");
public:
MedianFilter() = default;
/// Push one sample. Until N samples have been pushed the filter
/// returns the median over only the samples received so far.
T push(T sample) {
buffer_[write_idx_] = sample;
write_idx_ = (write_idx_ + 1) % N;
if (count_ < N) {
++count_;
}
return median();
}
/// Median of the current window (without pushing). Returns T{} if
/// no samples have been pushed yet.
T median() const {
if (count_ == 0) {
return T{};
}
std::array<T, N> sorted{};
for (std::size_t i = 0; i < count_; ++i) {
sorted[i] = buffer_[i];
}
std::sort(sorted.begin(), sorted.begin() + count_);
return sorted[count_ / 2];
}
/// Number of valid samples currently stored (0..N).
std::size_t size() const { return count_; }
/// True once the window has been filled at least once.
bool is_full() const { return count_ == N; }
/// Forget all samples; next push() starts fresh.
void reset() {
write_idx_ = 0;
count_ = 0;
buffer_.fill(T{});
}
private:
std::array<T, N> buffer_{};
std::size_t write_idx_{0};
std::size_t count_{0};
};
} // namespace arautopilot::filters
+158
View File
@@ -0,0 +1,158 @@
// =============================================================================
// di_do.cpp -- generic DI/DO implementation
// =============================================================================
#include "di_do.h"
#include <Arduino.h>
#include <array>
#include "../system/ar_log.h"
#include "pinout.h"
namespace arautopilot::hal {
namespace {
constexpr const char* TAG = "AR/HAL";
// Tunable: how many consecutive identical samples constitute a confirmed
// state for a DI. At a 50 Hz poll rate, 2 -> ~40 ms debounce.
constexpr uint8_t DI_DEBOUNCE_SAMPLES = 2;
struct DiSlot {
uint8_t pin;
bool state; // last confirmed (debounced) state
bool prev_state; // state on the *previous* poll, for edge detection
uint8_t stable_count; // consecutive identical raw reads
bool raw_last; // last raw read
};
constexpr std::size_t DI_COUNT = 5;
std::array<DiSlot, DI_COUNT> g_di_slots{
DiSlot{PIN_DI1_DISENGAGE_BUTTON, false, false, 0, false},
DiSlot{PIN_DI2_LIMIT_SWITCH_PORT, false, false, 0, false},
DiSlot{PIN_DI3_LIMIT_SWITCH_STBD, false, false, 0, false},
DiSlot{PIN_DI4_EXTERNAL_ALARM, false, false, 0, false},
DiSlot{PIN_DI5_MANUAL_CONFIRM, false, false, 0, false},
};
struct DoSlot {
uint8_t pin;
bool state;
};
constexpr std::size_t DO_COUNT = 10;
std::array<DoSlot, DO_COUNT> g_do_slots{
DoSlot{PIN_DO1_PUMP_PORT, false}, DoSlot{PIN_DO2_PUMP_STBD, false},
DoSlot{PIN_DO3_ACTUATOR_POWER, false}, DoSlot{PIN_DO4_BUZZER, false},
DoSlot{PIN_DO5_ENGAGED_LAMP, false}, DoSlot{PIN_DO6_RESERVED, false},
DoSlot{PIN_DO7_RESERVED, false}, DoSlot{PIN_DO8_RESERVED, false},
DoSlot{PIN_DO9_RESERVED, false}, DoSlot{PIN_DO10_RESERVED, false},
};
DiSlot* find_di(uint8_t pin) {
for (auto& slot : g_di_slots) {
if (slot.pin == pin) {
return &slot;
}
}
return nullptr;
}
DoSlot* find_do(uint8_t pin) {
for (auto& slot : g_do_slots) {
if (slot.pin == pin) {
return &slot;
}
}
return nullptr;
}
} // namespace
void di_init() {
for (auto& slot : g_di_slots) {
pinMode(slot.pin, INPUT_PULLUP);
// INPUT_PULLUP means a closed-to-ground switch reads LOW=pressed.
// Our logical "true" = "pressed/active", so we invert in di_poll().
slot.state = false;
slot.prev_state = false;
slot.stable_count = 0;
slot.raw_last = false;
}
AR_LOGI(TAG, "di_init: %u digital inputs configured (INPUT_PULLUP)",
(unsigned)g_di_slots.size());
}
void di_poll() {
for (auto& slot : g_di_slots) {
// Active-low (INPUT_PULLUP + switch-to-GND).
bool raw = (digitalRead(slot.pin) == LOW);
slot.prev_state = slot.state;
if (raw == slot.raw_last) {
if (slot.stable_count < DI_DEBOUNCE_SAMPLES) {
++slot.stable_count;
}
if (slot.stable_count >= DI_DEBOUNCE_SAMPLES) {
slot.state = raw;
}
} else {
slot.stable_count = 0;
}
slot.raw_last = raw;
}
}
bool di_read(uint8_t pin) {
auto* slot = find_di(pin);
return slot != nullptr ? slot->state : false;
}
bool di_rising_edge(uint8_t pin) {
auto* slot = find_di(pin);
return slot != nullptr && slot->state && !slot->prev_state;
}
bool di_falling_edge(uint8_t pin) {
auto* slot = find_di(pin);
return slot != nullptr && !slot->state && slot->prev_state;
}
void do_init() {
for (auto& slot : g_do_slots) {
pinMode(slot.pin, OUTPUT);
digitalWrite(slot.pin, LOW);
slot.state = false;
}
AR_LOGI(TAG, "do_init: %u digital outputs configured (driven LOW)",
(unsigned)g_do_slots.size());
}
bool do_write(uint8_t pin, bool high) {
auto* slot = find_do(pin);
if (slot == nullptr) {
AR_LOGW(TAG, "do_write: unknown pin %d", (int)pin);
return false;
}
if (slot->state == high) {
return false;
}
digitalWrite(slot->pin, high ? HIGH : LOW);
slot->state = high;
return true;
}
bool do_state(uint8_t pin) {
auto* slot = find_do(pin);
return slot != nullptr ? slot->state : false;
}
void do_all_off() {
for (auto& slot : g_do_slots) {
digitalWrite(slot.pin, LOW);
slot.state = false;
}
AR_LOGW(TAG, "do_all_off: all digital outputs driven LOW");
}
} // namespace arautopilot::hal
+57
View File
@@ -0,0 +1,57 @@
// =============================================================================
// di_do.h -- generic digital-input / digital-output helpers
// =============================================================================
//
// Thin layer above Arduino digitalRead / digitalWrite that:
// - Tracks the *logical* state of every input/output so other tasks can
// query without re-reading the pin.
// - Debounces DIs in software (configurable, default 20 ms).
// - Caches the last commanded DO state so we never write the same value
// twice (cheap optimisation for slow open-drain outputs).
//
// Pins handled by this module are the ones listed in hal/pinout.h.
// =============================================================================
#pragma once
#include <cstdint>
namespace arautopilot::hal {
// ----- Digital inputs -------------------------------------------------------
/// Initialise all DI pins declared in pinout.h with INPUT_PULLUP.
/// Must be called once during setup() before any di_read() call.
void di_init();
/// Sample every DI once, run the debounce filter, and store the result.
/// Intended to be called from the safety task at a fixed rate (50 Hz).
void di_poll();
/// Return the last debounced logical state of a DI pin.
/// Pin must be one of the PIN_DIx_* constants from pinout.h.
bool di_read(uint8_t pin);
/// Return true if the pin changed state on the most recent di_poll() call
/// (edge-detect). Useful for the disengage button.
bool di_rising_edge(uint8_t pin);
bool di_falling_edge(uint8_t pin);
// ----- Digital outputs ------------------------------------------------------
/// Initialise all DO pins declared in pinout.h as OUTPUT and drive them LOW.
/// Must be called once during setup() before any do_write() call.
void do_init();
/// Set a DO pin to the given logical state. No-op if the pin was already in
/// that state. Returns true if the write actually happened.
/// Pin must be one of the PIN_DOx_* constants from pinout.h.
bool do_write(uint8_t pin, bool high);
/// Return the last commanded state of a DO pin.
bool do_state(uint8_t pin);
/// Drive every DO LOW. Called by the safety system on emergency disengage.
void do_all_off();
} // namespace arautopilot::hal
@@ -0,0 +1,115 @@
// =============================================================================
// rudder_actuator.cpp -- rudder actuator driver (Sprint 1 stub)
// =============================================================================
#include "rudder_actuator.h"
#include <Arduino.h>
#include "../modes/standby.h"
#include "../system/ar_log.h"
#include "di_do.h"
#include "pinout.h"
namespace arautopilot::hal {
namespace {
constexpr const char* TAG = "AR/HAL";
bool g_power_on = false;
int8_t g_last_command_pct = 0;
} // namespace
void rudder_actuator_init() {
// do_init() in di_do.cpp already configured DO1..DO10 as outputs LOW.
// Just make sure our local state matches and assert the safe defaults.
do_write(PIN_DO1_PUMP_PORT, false);
do_write(PIN_DO2_PUMP_STBD, false);
do_write(PIN_DO3_ACTUATOR_POWER, false);
g_power_on = false;
g_last_command_pct = 0;
AR_LOGI(TAG, "rudder_actuator_init: power OFF, both directions LOW");
}
void rudder_actuator_power_on() {
do_write(PIN_DO1_PUMP_PORT, false); // ensure direction outputs LOW before
do_write(PIN_DO2_PUMP_STBD, false); // we energise the relay
do_write(PIN_DO3_ACTUATOR_POWER, true);
g_power_on = true;
AR_LOGI(TAG, "rudder_actuator: master power ON");
}
void rudder_actuator_power_off() {
do_write(PIN_DO1_PUMP_PORT, false);
do_write(PIN_DO2_PUMP_STBD, false);
do_write(PIN_DO3_ACTUATOR_POWER, false);
g_power_on = false;
g_last_command_pct = 0;
AR_LOGW(TAG, "rudder_actuator: master power OFF (interlock or operator)");
}
bool rudder_actuator_is_powered() { return g_power_on; }
bool rudder_actuator_at_limit() {
return di_read(PIN_DI2_LIMIT_SWITCH_PORT) ||
di_read(PIN_DI3_LIMIT_SWITCH_STBD);
}
bool rudder_command(int8_t pwm_pct) {
// ---- Safety interlocks -------------------------------------------------
// Interlock #1: master power must be on. Without DO3, the H-bridge or
// pump relays are isolated and the direction outputs do nothing -- but
// we refuse anyway so the firmware state is consistent.
if (!g_power_on) {
if (pwm_pct != 0) {
AR_LOGW(TAG, "rudder_command(%d): refused -- power OFF",
(int)pwm_pct);
}
do_write(PIN_DO1_PUMP_PORT, false);
do_write(PIN_DO2_PUMP_STBD, false);
g_last_command_pct = 0;
return false;
}
// Interlock #2: STANDBY mode never drives the rudder.
if (modes::is_standby()) {
if (pwm_pct != 0) {
AR_LOGW(TAG, "rudder_command(%d): refused -- STANDBY", (int)pwm_pct);
}
do_write(PIN_DO1_PUMP_PORT, false);
do_write(PIN_DO2_PUMP_STBD, false);
g_last_command_pct = 0;
return false;
}
// Interlock #3: limit switches block further travel in that direction.
if (pwm_pct < 0 && di_read(PIN_DI2_LIMIT_SWITCH_PORT)) {
AR_LOGW(TAG, "rudder_command(%d): blocked -- port limit", (int)pwm_pct);
do_write(PIN_DO1_PUMP_PORT, false);
return false;
}
if (pwm_pct > 0 && di_read(PIN_DI3_LIMIT_SWITCH_STBD)) {
AR_LOGW(TAG, "rudder_command(%d): blocked -- starboard limit",
(int)pwm_pct);
do_write(PIN_DO2_PUMP_STBD, false);
return false;
}
// ---- Direction output --------------------------------------------------
// Sprint 1 stub: just toggle the direction outputs. No PWM modulation;
// the intensity will be wired in Sprint 2 via LEDC.
if (pwm_pct > 0) {
do_write(PIN_DO1_PUMP_PORT, false);
do_write(PIN_DO2_PUMP_STBD, true);
} else if (pwm_pct < 0) {
do_write(PIN_DO2_PUMP_STBD, false);
do_write(PIN_DO1_PUMP_PORT, true);
} else {
do_write(PIN_DO1_PUMP_PORT, false);
do_write(PIN_DO2_PUMP_STBD, false);
}
g_last_command_pct = pwm_pct;
return true;
}
} // namespace arautopilot::hal
@@ -0,0 +1,52 @@
// =============================================================================
// rudder_actuator.h -- rudder actuator driver (Sprint 1 stub)
// =============================================================================
//
// Drives the rudder pump/motor via DO1 (port direction), DO2 (starboard
// direction), and DO3 (master power relay). The actual command output is
// produced by the inner PID loop (Sprint 2). In Sprint 1 this module:
//
// - Exposes a `rudder_command(int8_t pwm_pct)` API.
// - Refuses to act if the rudder is at its mechanical limit (DI2/DI3).
// - Refuses to act if master power is off (DO3 LOW).
// - Refuses to act if the system is in STANDBY (Sprint 1 default).
//
// All three "refuse" conditions are safety-critical: they remain in place
// for every subsequent sprint.
// =============================================================================
#pragma once
#include <cstdint>
namespace arautopilot::hal {
/// Configure DO1/DO2/DO3 as outputs and drive them all LOW.
void rudder_actuator_init();
/// Engage the master power relay (DO3 HIGH). Required before any
/// rudder_command() call has effect.
void rudder_actuator_power_on();
/// Drop the master power relay and stop both directions. Idempotent.
void rudder_actuator_power_off();
/// Send a signed command to the actuator:
/// pwm_pct = 0 -> both direction outputs LOW (rudder freewheels)
/// pwm_pct > 0 -> drive STARBOARD (DO2 HIGH)
/// pwm_pct < 0 -> drive PORT (DO1 HIGH)
///
/// Sprint 1 stub: only the direction outputs are toggled, no PWM modulation
/// (intensity ignored). Sprint 2 will replace the body with a real LEDC PWM.
///
/// Returns true if the command was actually applied; false if a safety
/// interlock blocked it (limit switch, power off, or standby mode).
bool rudder_command(int8_t pwm_pct);
/// True if the master power relay is currently engaged.
bool rudder_actuator_is_powered();
/// True if either limit switch is asserted.
bool rudder_actuator_at_limit();
} // namespace arautopilot::hal
@@ -0,0 +1,107 @@
// =============================================================================
// rudder_sensor.cpp -- AI1 rudder-angle sensor with median filter
// =============================================================================
#include "rudder_sensor.h"
#include <Arduino.h>
#include "../filters/median.h"
#include "../system/ar_log.h"
#include "../system/task_config.h"
#include "pinout.h"
namespace arautopilot::hal {
namespace {
constexpr const char* TAG = "AR/HAL";
// Calibration defaults: full-range ADC mapped to +-35 deg of rudder.
// Reasonable for an unconfigured bench but NEVER ship this to a customer
// vessel -- it must be replaced during sea-trial commissioning (Sprint 7).
constexpr int16_t DEFAULT_RAW_AT_MIN = 0;
constexpr int16_t DEFAULT_RAW_AT_MAX = 4095;
constexpr float DEFAULT_MIN_DEG = -35.0f;
constexpr float DEFAULT_MAX_DEG = +35.0f;
filters::MedianFilter<int16_t, 5> g_median{};
portMUX_TYPE g_mux = portMUX_INITIALIZER_UNLOCKED;
RudderReading g_latest{0, 0.0f, 0, false};
struct Calibration {
int16_t raw_at_min;
int16_t raw_at_max;
float min_deg;
float max_deg;
};
Calibration g_calib{DEFAULT_RAW_AT_MIN, DEFAULT_RAW_AT_MAX, DEFAULT_MIN_DEG,
DEFAULT_MAX_DEG};
float raw_to_deg(int16_t raw, const Calibration& c) {
const float span_raw = static_cast<float>(c.raw_at_max - c.raw_at_min);
if (span_raw == 0.0f) {
return 0.0f;
}
const float t = (static_cast<float>(raw - c.raw_at_min)) / span_raw;
return c.min_deg + t * (c.max_deg - c.min_deg);
}
void SensorTask(void* /*pv*/) {
AR_LOGI(TAG, "rudder_sensor task started on core %d, pin %d (ADC1)",
xPortGetCoreID(), PIN_AI1_RUDDER_ANGLE);
TickType_t last_wake = xTaskGetTickCount();
for (;;) {
const int raw = analogRead(PIN_AI1_RUDDER_ANGLE);
const int16_t filtered = g_median.push(static_cast<int16_t>(raw));
Calibration cal;
portENTER_CRITICAL(&g_mux);
cal = g_calib;
portEXIT_CRITICAL(&g_mux);
const float angle = raw_to_deg(filtered, cal);
portENTER_CRITICAL(&g_mux);
g_latest.raw_adc = filtered;
g_latest.angle_deg = angle;
g_latest.timestamp_ms = millis();
g_latest.valid = g_median.is_full();
portEXIT_CRITICAL(&g_mux);
vTaskDelayUntil(&last_wake, pdMS_TO_TICKS(AR_PERIOD_MS_RUDDER_SENSOR));
}
}
} // namespace
void rudder_sensor_init() {
analogReadResolution(12); // 0..4095
analogSetAttenuation(ADC_11db); // ~0..3.3 V input range
g_median.reset();
AR_LOGI(TAG, "rudder_sensor_init: 12-bit ADC, 11dB attn, %d-sample median",
5);
}
void rudder_sensor_start_task() {
xTaskCreatePinnedToCore(SensorTask, "rudder_sensor",
AR_TASK_STACK_RUDDER_SENSOR, nullptr,
AR_TASK_PRIO_RUDDER_SENSOR, nullptr,
AR_TASK_CORE_REALTIME);
}
RudderReading rudder_sensor_latest() {
RudderReading copy;
portENTER_CRITICAL(&g_mux);
copy = g_latest;
portEXIT_CRITICAL(&g_mux);
return copy;
}
void rudder_sensor_set_calibration(int16_t raw_at_min_deg, int16_t raw_at_max_deg,
float min_deg, float max_deg) {
portENTER_CRITICAL(&g_mux);
g_calib = {raw_at_min_deg, raw_at_max_deg, min_deg, max_deg};
portEXIT_CRITICAL(&g_mux);
AR_LOGI(TAG,
"rudder_sensor calibration updated: raw [%d..%d] -> deg [%.2f..%.2f]",
raw_at_min_deg, raw_at_max_deg, min_deg, max_deg);
}
} // namespace arautopilot::hal
@@ -0,0 +1,47 @@
// =============================================================================
// rudder_sensor.h -- AI1 rudder-angle sensor with median filter
// =============================================================================
//
// Reads the raw ADC value of the rudder position sensor (pot, Hall, or
// 4-20 mA loop conditioned to 0-3.3 V) on PIN_AI1_RUDDER_ANGLE, applies a
// 5-sample median filter to suppress single-sample spikes, and converts the
// result to degrees via a linear calibration.
//
// Calibration in Sprint 1 is a hard-coded placeholder (-35 deg @ 0 raw,
// +35 deg @ 4095 raw). In Sprint 7 (commissioning), the calibration values
// will come from the persistent NVS store written during sea trial.
//
// The sensor task runs at 100 Hz on Core 1 (real-time core).
// =============================================================================
#pragma once
#include <cstdint>
namespace arautopilot::hal {
struct RudderReading {
int16_t raw_adc; ///< 0..4095, raw ADC after median filter
float angle_deg; ///< -35.0 .. +35.0 typical, after calibration
uint32_t timestamp_ms; ///< millis() at which the sample was taken
bool valid; ///< false until the filter has filled
};
/// Configure ADC1 channel for AI1, init the median filter.
void rudder_sensor_init();
/// Start the FreeRTOS sampling task (100 Hz, Core 1).
void rudder_sensor_start_task();
/// Get the latest filtered reading. Thread-safe (single critical section).
RudderReading rudder_sensor_latest();
/// Override the linear calibration. Called by the commissioning code
/// (Sprint 7); the placeholder is fine for Sprint 1 bench work.
///
/// raw_at_min_deg, raw_at_max_deg : ADC counts (0..4095)
/// min_deg, max_deg : physical angle in degrees
void rudder_sensor_set_calibration(int16_t raw_at_min_deg, int16_t raw_at_max_deg,
float min_deg, float max_deg);
} // namespace arautopilot::hal
+98
View File
@@ -0,0 +1,98 @@
// =============================================================================
// AR-Autopilot v1 -- main.cpp
// =============================================================================
//
// Sprint 1 firmware entry point. Boots in STANDBY mode, spawns the FreeRTOS
// tasks declared in system/task_config.h, and returns control to the Arduino
// scheduler. The loop() function intentionally does nothing -- every long-
// running activity lives in a pinned task.
//
// Task layout summary (full table in system/task_config.h):
//
// Core 1 (real-time): PID inner, PID outer, rudder sensor, safety
// Core 0 (comms): NMEA 2000 RX, Modbus slave, heartbeat, health
//
// Sprint 1 boots only:
// - heartbeat (Core 0) -- LED + uptime log
//
// Later sprints will register the rest from this same setup() function. The
// task_config.h header already reserves their priorities/stacks/cores.
// =============================================================================
#include <Arduino.h>
#include "hal/di_do.h"
#include "hal/pinout.h"
#include "hal/rudder_actuator.h"
#include "hal/rudder_sensor.h"
#include "modes/standby.h"
#include "protocols/modbus_slave.h"
#include "protocols/nmea2000_consumer.h"
#include "safety/safety_monitor.h"
#include "safety/watchdog.h"
#include "system/ar_log.h"
#include "system/task_config.h"
// Forward declarations of task-spawning helpers (defined in their own .cpp
// files). Keeping main.cpp dependency-free of internals lets each subsystem
// own its own task setup code.
extern void ar_start_heartbeat_task();
namespace {
constexpr const char* TAG = "AR/MAIN";
} // namespace
void setup() {
// Wait for the USB CDC serial port to be ready before we start logging.
Serial.begin(115200);
delay(200);
AR_LOGI(TAG, "================================================");
AR_LOGI(TAG, " %s -- firmware boot", AR_AUTOPILOT_FW_NAME);
AR_LOGI(TAG, " version : %s", AR_FW_VERSION);
AR_LOGI(TAG, " variant : %s", AR_BUILD_VARIANT);
AR_LOGI(TAG, " build : %s", AR_FW_BUILD_TIMESTAMP);
AR_LOGI(TAG, " board : %s", AR_AUTOPILOT_HW_BOARD);
AR_LOGI(TAG, " mcu : %s @ %d MHz", AR_AUTOPILOT_MCU,
(int)ESP.getCpuFreqMHz());
AR_LOGI(TAG, " cores : %d free heap: %u bytes",
(int)ESP.getChipCores(), ESP.getFreeHeap());
AR_LOGI(TAG, "================================================");
// Initialise the pilot mode state machine (boots in STANDBY).
arautopilot::modes::mode_init();
// Initialise hardware abstraction layer.
arautopilot::hal::di_init();
arautopilot::hal::do_init();
arautopilot::hal::rudder_sensor_init();
arautopilot::hal::rudder_actuator_init();
// Safety: watchdog + DI override task. Initialised first so the
// watchdog is armed before slower subsystems come up.
arautopilot::safety::watchdog_init();
AR_LOGI(TAG, "spawning Sprint 1 tasks ...");
arautopilot::safety::safety_monitor_start_task();
arautopilot::hal::rudder_sensor_start_task();
ar_start_heartbeat_task();
// Modbus slave (server) -- exposes telemetry + commands to the display.
arautopilot::protocols::modbus::modbus_slave_init();
arautopilot::protocols::modbus::modbus_slave_start();
// NMEA 2000 consumer (PGN 127250 + 127251 in Sprint 1).
arautopilot::protocols::nmea2000::nmea2000_consumer_init();
arautopilot::protocols::nmea2000::nmea2000_consumer_start_task();
AR_LOGI(TAG, "setup() complete; control loop is FreeRTOS-driven.");
AR_LOGI(TAG, "current mode: STANDBY (helm is manual)");
}
void loop() {
// Intentionally empty. All real work happens in FreeRTOS tasks.
// The Arduino loopTask itself runs at priority 1 on Core 1 by default;
// we yield generously to keep it out of the way of the real-time tasks.
vTaskDelay(pdMS_TO_TICKS(1000));
}
@@ -0,0 +1,80 @@
// =============================================================================
// modes/standby.cpp -- pilot mode state (Sprint 1)
// =============================================================================
#include "standby.h"
#include <Arduino.h>
#include "../system/ar_log.h"
namespace arautopilot::modes {
namespace {
constexpr const char* TAG = "AR/MODE";
portMUX_TYPE g_mux = portMUX_INITIALIZER_UNLOCKED;
Mode g_mode = Mode::STANDBY;
const char* mode_name(Mode m) {
switch (m) {
case Mode::STANDBY: return "STANDBY";
case Mode::HEADING_HOLD: return "HEADING_HOLD";
case Mode::TRUE_COURSE: return "TRUE_COURSE";
case Mode::TRACK_KEEPING: return "TRACK_KEEPING";
case Mode::DODGE: return "DODGE";
}
return "UNKNOWN";
}
} // namespace
void mode_init() {
portENTER_CRITICAL(&g_mux);
g_mode = Mode::STANDBY;
portEXIT_CRITICAL(&g_mux);
AR_LOGI(TAG, "mode_init: %s", mode_name(g_mode));
}
Mode current_mode() {
portENTER_CRITICAL(&g_mux);
Mode m = g_mode;
portEXIT_CRITICAL(&g_mux);
return m;
}
bool is_standby() { return current_mode() == Mode::STANDBY; }
bool request_mode(Mode m) {
// Sprint 1: only STANDBY is reachable. The other modes exist in the enum
// for forward compatibility (Modbus already has slots for them) but the
// PID and modes machinery is not in place yet.
if (m == Mode::STANDBY) {
portENTER_CRITICAL(&g_mux);
Mode prev = g_mode;
g_mode = Mode::STANDBY;
portEXIT_CRITICAL(&g_mux);
if (prev != Mode::STANDBY) {
AR_LOGI(TAG, "mode change: %s -> STANDBY", mode_name(prev));
}
return true;
}
AR_LOGW(TAG,
"request_mode(%s) rejected: only STANDBY is implemented in "
"Sprint 1; current mode remains %s",
mode_name(m), mode_name(current_mode()));
return false;
}
void force_standby(const char* reason) {
portENTER_CRITICAL(&g_mux);
Mode prev = g_mode;
g_mode = Mode::STANDBY;
portEXIT_CRITICAL(&g_mux);
if (prev != Mode::STANDBY) {
AR_LOGE(TAG, "force_standby: %s -> STANDBY (reason: %s)",
mode_name(prev), reason != nullptr ? reason : "unspecified");
}
}
} // namespace arautopilot::modes
@@ -0,0 +1,46 @@
// =============================================================================
// modes/standby.h -- pilot mode state (Sprint 1)
// =============================================================================
//
// Holds the global "what mode is the pilot in" flag. In Sprint 1 the only
// mode that does anything real is STANDBY. The other Phase 1 modes
// (HEADING_HOLD, TRUE_COURSE, TRACK_KEEPING, DODGE) are reserved in the
// enum but cannot be entered yet -- attempting to set them logs a warning
// and stays in STANDBY.
//
// Later sprints expand this module into a proper state machine driven by
// the safety system and the operator's Modbus commands.
// =============================================================================
#pragma once
#include <cstdint>
namespace arautopilot::modes {
enum class Mode : uint8_t {
STANDBY = 0,
HEADING_HOLD = 1,
TRUE_COURSE = 2,
TRACK_KEEPING = 3,
DODGE = 4,
};
/// Initialise to STANDBY. Must be called once from setup().
void mode_init();
/// Atomically read the current mode.
Mode current_mode();
/// True if and only if current_mode() == STANDBY.
bool is_standby();
/// Try to enter `m`. In Sprint 1 only STANDBY is accepted; anything else
/// is rejected with a warning. Returns true on success.
bool request_mode(Mode m);
/// Force-return to STANDBY (called by the safety system on auto-disengage,
/// watchdog reset, or the DI1 physical button).
void force_standby(const char* reason);
} // namespace arautopilot::modes
@@ -0,0 +1,148 @@
// =============================================================================
// modbus_registers.h -- AR-Autopilot Modbus RTU register map
// =============================================================================
//
// AUTO-GENERATED. Do not edit by hand.
// Source: firmware/ar_autopilot_v1/modbus_registers.yaml
// Regenerate with: python tools/gen_modbus_registers.py
// =============================================================================
#pragma once
#include <cstdint>
namespace arautopilot::protocols::modbus {
constexpr const char* MAP_SCHEMA_VERSION = "0.1.0";
constexpr uint8_t SLAVE_ID = 1;
constexpr uint32_t BAUDRATE = 38400;
constexpr char PARITY = 'N';
constexpr uint8_t DATA_BITS = 8;
constexpr uint8_t STOP_BITS = 1;
// ----- Discrete inputs (read-only bits) -----
constexpr uint16_t DISCRETE_COUNT = 19;
constexpr uint16_t DISCRETE_MAX_ADDR = 25;
// 1 if the pilot is currently engaged (any mode other than STANDBY)
constexpr uint16_t DISCRETE_PILOT_ENGAGED = 0;
// Live state of the physical Engage/Disengage push-button
constexpr uint16_t DISCRETE_DI_DISENGAGE_BUTTON = 1;
// Port-side rudder mechanical end-stop reached
constexpr uint16_t DISCRETE_DI_LIMIT_PORT = 2;
// Starboard-side rudder mechanical end-stop reached
constexpr uint16_t DISCRETE_DI_LIMIT_STBD = 3;
// External critical alarm (VMS / genset) asserted
constexpr uint16_t DISCRETE_DI_EXTERNAL_ALARM = 4;
// Manual confirmation switch asserted (emergency override)
constexpr uint16_t DISCRETE_DI_MANUAL_CONFIRM = 5;
// Master actuator power relay (DO3) commanded ON
constexpr uint16_t DISCRETE_ACTUATOR_POWER = 8;
// Actuator direction output: driving to port
constexpr uint16_t DISCRETE_ACTUATOR_DRIVING_PORT = 9;
// Actuator direction output: driving to starboard
constexpr uint16_t DISCRETE_ACTUATOR_DRIVING_STBD = 10;
// Off-course warning active
constexpr uint16_t DISCRETE_ALARM_OFF_COURSE = 16;
// Severe off-course alarm (auto-disengage)
constexpr uint16_t DISCRETE_ALARM_OFF_COURSE_SEVERE = 17;
// Rudder command sent but no feedback motion
constexpr uint16_t DISCRETE_ALARM_RUDDER_NOT_RESP = 18;
// NMEA 2000 heading PGN not received >5 s
constexpr uint16_t DISCRETE_ALARM_HEADING_LOST = 19;
// Actuator current over threshold
constexpr uint16_t DISCRETE_ALARM_ACTUATOR_OVERCURR = 20;
// Supply voltage below safe threshold
constexpr uint16_t DISCRETE_ALARM_VOLTAGE_LOW = 21;
// Rudder reached mechanical end-stop
constexpr uint16_t DISCRETE_ALARM_LIMIT_REACHED = 22;
// Firmware watchdog fired -- controller reset
constexpr uint16_t DISCRETE_ALARM_WATCHDOG_TRIPPED = 23;
// VMS reported blackout or electrical fault
constexpr uint16_t DISCRETE_ALARM_VMS_CRITICAL = 24;
// OR of all alarm bits (convenience)
constexpr uint16_t DISCRETE_ANY_ALARM_ACTIVE = 25;
// ----- Coils (read-write bits) -----
constexpr uint16_t COIL_COUNT = 4;
constexpr uint16_t COIL_MAX_ADDR = 3;
// Rising edge requests pilot engagement (subject to interlocks)
constexpr uint16_t COIL_CMD_ENGAGE_REQUEST = 0;
// Rising edge forces pilot to STANDBY
constexpr uint16_t COIL_CMD_DISENGAGE_REQUEST = 1;
// Rising edge acknowledges every active alarm
constexpr uint16_t COIL_CMD_ACK_ALL_ALARMS = 2;
// Knob arming request (Sprint 7+)
constexpr uint16_t COIL_CMD_KNOB_ARM = 3;
// ----- Input registers (read-only words) -----
constexpr uint16_t INPUT_COUNT = 17;
constexpr uint16_t INPUT_MAX_ADDR = 33;
// Firmware major version
constexpr uint16_t INPUT_FW_VERSION_MAJOR = 0;
// Firmware minor version
constexpr uint16_t INPUT_FW_VERSION_MINOR = 1;
// Firmware patch version
constexpr uint16_t INPUT_FW_VERSION_PATCH = 2;
// Modbus map schema version (0=v0.1.0)
constexpr uint16_t INPUT_SCHEMA_VERSION = 3;
// Uptime seconds, low 16 bits
// unit=s
constexpr uint16_t INPUT_UPTIME_SECONDS_LO = 4;
// Uptime seconds, high 16 bits
// unit=s
constexpr uint16_t INPUT_UPTIME_SECONDS_HI = 5;
// Current AutopilotMode (0=STANDBY,1=HH,2=TC,3=TK,4=DODGE)
constexpr uint16_t INPUT_CURRENT_MODE = 6;
// Current free heap, KiB
// unit=KiB
constexpr uint16_t INPUT_FREE_HEAP_KB = 7;
// Minimum free heap since boot
// unit=KiB
constexpr uint16_t INPUT_MIN_FREE_HEAP_KB = 8;
// Filtered rudder angle, deg * 100 (-3500..+3500)
// unit=deg, scale=0.01
constexpr uint16_t INPUT_RUDDER_ANGLE_DEG_X100 = 16;
// Raw ADC reading after median filter (0..4095)
// unit=counts
constexpr uint16_t INPUT_RUDDER_RAW_ADC = 17;
// 1 if median filter has filled (>=5 samples)
constexpr uint16_t INPUT_RUDDER_VALID = 18;
// Current heading from NMEA 2000 PGN 127250, deg*100 (0..35999)
// unit=deg, scale=0.01
constexpr uint16_t INPUT_HEADING_DEG_X100 = 24;
// Rate of turn from PGN 127251, deg/s*100 (signed int16)
// unit=deg/s, scale=0.01
constexpr uint16_t INPUT_ROT_DPS_X100 = 25;
// Milliseconds since the last heading update (0..60000)
// unit=ms
constexpr uint16_t INPUT_HEADING_AGE_MS = 26;
// System battery voltage, V*100
// unit=V, scale=0.01
constexpr uint16_t INPUT_BATTERY_VOLTAGE_X100 = 32;
// Actuator current, A*100
// unit=A, scale=0.01
constexpr uint16_t INPUT_ACTUATOR_CURRENT_X100 = 33;
// ----- Holding registers (read-write words) -----
constexpr uint16_t HOLDING_COUNT = 5;
constexpr uint16_t HOLDING_MAX_ADDR = 8;
// Mode requested by operator (0=STANDBY,1=HH,2=TC,3=TK,4=DODGE)
constexpr uint16_t HOLDING_MODE_REQUEST = 0;
// Desired heading, deg*100
// unit=deg, scale=0.01
constexpr uint16_t HOLDING_HEADING_SETPOINT_X100 = 1;
// Display brightness 0..100
// unit=%
constexpr uint16_t HOLDING_BRIGHTNESS_PCT = 2;
// Alarm volume 0..100
// unit=%
constexpr uint16_t HOLDING_ALARM_VOLUME_PCT = 3;
// Dodge mode heading offset, deg*100 (signed int16)
// unit=deg, scale=0.01
constexpr uint16_t HOLDING_DODGE_OFFSET_DEG_X100 = 8;
} // namespace arautopilot::protocols::modbus
@@ -0,0 +1,382 @@
// =============================================================================
// modbus_slave.cpp -- eModbus-based RTU server (slave) implementation
// =============================================================================
//
// Sprint 1 scope:
// - Input registers (FC 0x04): firmware version, uptime, mode, heap,
// rudder angle/raw/valid, heading + ROT (stub for Sprint 1), battery
// and actuator current placeholders.
// - Discrete inputs (FC 0x02): engaged flag, all DIs, alarm bits.
// - Holding registers (FC 0x03/0x06/0x10): mode request, heading
// setpoint, brightness, alarm volume, dodge offset.
// - Coils (FC 0x01/0x05/0x0F): engage/disengage requests, ack-all,
// knob arm (reserved).
//
// In Sprint 1 the writes that try to change to a non-STANDBY mode are
// silently coerced (the modes::request_mode() helper rejects them with a
// warning).
// =============================================================================
#include "modbus_slave.h"
#include <Arduino.h>
#include <ModbusServerRTU.h>
#include "../hal/di_do.h"
#include "../hal/pinout.h"
#include "../hal/rudder_sensor.h"
#include "../modes/standby.h"
#include "../system/ar_log.h"
#include "../system/task_config.h"
#include "modbus_registers.h"
#include "nmea2000_consumer.h"
namespace arautopilot::protocols::modbus {
namespace {
constexpr const char* TAG = "AR/MB";
// eModbus server with a 1000 ms timeout for client transactions.
ModbusServerRTU g_server(1000, PIN_RS485_DE);
bool g_running = false;
volatile uint32_t g_req_count = 0;
volatile uint32_t g_err_count = 0;
// ----- Storage for the writable side (coils + holding registers) -----------
// Discrete inputs and input registers are computed on the fly from the live
// telemetry helpers, so they don't need backing storage. Coils and holding
// registers do (eModbus expects deterministic reads of the values it last
// stored).
struct HoldingStorage {
uint16_t mode_request = 0;
int16_t heading_setpoint_x100 = 0;
uint16_t brightness_pct = 80;
uint16_t alarm_volume_pct = 60;
int16_t dodge_offset_deg_x100 = 0;
};
HoldingStorage g_holding;
struct CoilStorage {
bool engage_request = false;
bool disengage_request = false;
bool ack_all = false;
bool knob_arm = false;
};
CoilStorage g_coils;
// ----- Helpers ---------------------------------------------------------------
uint16_t read_input_register(uint16_t addr) {
switch (addr) {
case INPUT_FW_VERSION_MAJOR: return 0;
case INPUT_FW_VERSION_MINOR: return 1;
case INPUT_FW_VERSION_PATCH: return 0;
case INPUT_SCHEMA_VERSION: return 0;
case INPUT_UPTIME_SECONDS_LO: return (uint16_t)((millis() / 1000U) & 0xFFFFU);
case INPUT_UPTIME_SECONDS_HI: return (uint16_t)(((millis() / 1000U) >> 16) & 0xFFFFU);
case INPUT_CURRENT_MODE: return (uint16_t)modes::current_mode();
case INPUT_FREE_HEAP_KB: return (uint16_t)(ESP.getFreeHeap() / 1024U);
case INPUT_MIN_FREE_HEAP_KB: return (uint16_t)(ESP.getMinFreeHeap() / 1024U);
case INPUT_RUDDER_ANGLE_DEG_X100: {
auto r = hal::rudder_sensor_latest();
int v = (int)(r.angle_deg * 100.0f);
if (v < -32768) v = -32768;
if (v > 32767) v = 32767;
return (uint16_t)(int16_t)v;
}
case INPUT_RUDDER_RAW_ADC: {
auto r = hal::rudder_sensor_latest();
return (uint16_t)r.raw_adc;
}
case INPUT_RUDDER_VALID: {
auto r = hal::rudder_sensor_latest();
return r.valid ? 1 : 0;
}
case INPUT_HEADING_DEG_X100: {
auto n = nmea2000::nmea2000_latest();
int v = (int)(n.heading_deg * 100.0f);
if (v < 0) v = 0;
if (v > 35999) v = 35999;
return (uint16_t)v;
}
case INPUT_ROT_DPS_X100: {
auto n = nmea2000::nmea2000_latest();
int v = (int)(n.rate_of_turn_dps * 100.0f);
if (v < -32768) v = -32768;
if (v > 32767) v = 32767;
return (uint16_t)(int16_t)v;
}
case INPUT_HEADING_AGE_MS: {
auto n = nmea2000::nmea2000_latest();
uint32_t age = (millis() - n.heading_age_ms);
if (!n.heading_valid) age = 60000;
if (age > 60000) age = 60000;
return (uint16_t)age;
}
// Sprint 1: battery voltage and actuator current wired in Sprint 6
// (Safety + alarms). For now, return 0.
case INPUT_BATTERY_VOLTAGE_X100:
case INPUT_ACTUATOR_CURRENT_X100:
return 0;
default:
return 0;
}
}
bool read_discrete(uint16_t addr) {
switch (addr) {
case DISCRETE_PILOT_ENGAGED: return !modes::is_standby();
case DISCRETE_DI_DISENGAGE_BUTTON: return hal::di_read(PIN_DI1_DISENGAGE_BUTTON);
case DISCRETE_DI_LIMIT_PORT: return hal::di_read(PIN_DI2_LIMIT_SWITCH_PORT);
case DISCRETE_DI_LIMIT_STBD: return hal::di_read(PIN_DI3_LIMIT_SWITCH_STBD);
case DISCRETE_DI_EXTERNAL_ALARM: return hal::di_read(PIN_DI4_EXTERNAL_ALARM);
case DISCRETE_DI_MANUAL_CONFIRM: return hal::di_read(PIN_DI5_MANUAL_CONFIRM);
case DISCRETE_ACTUATOR_POWER: return hal::do_state(PIN_DO3_ACTUATOR_POWER);
case DISCRETE_ACTUATOR_DRIVING_PORT:return hal::do_state(PIN_DO1_PUMP_PORT);
case DISCRETE_ACTUATOR_DRIVING_STBD:return hal::do_state(PIN_DO2_PUMP_STBD);
// Alarm bits: stubs in Sprint 1, wired in Sprint 6.
case DISCRETE_ALARM_OFF_COURSE:
case DISCRETE_ALARM_OFF_COURSE_SEVERE:
case DISCRETE_ALARM_RUDDER_NOT_RESP:
case DISCRETE_ALARM_HEADING_LOST:
case DISCRETE_ALARM_ACTUATOR_OVERCURR:
case DISCRETE_ALARM_VOLTAGE_LOW:
case DISCRETE_ALARM_LIMIT_REACHED:
case DISCRETE_ALARM_WATCHDOG_TRIPPED:
case DISCRETE_ALARM_VMS_CRITICAL:
case DISCRETE_ANY_ALARM_ACTIVE:
return false;
default:
return false;
}
}
uint16_t read_holding(uint16_t addr) {
switch (addr) {
case HOLDING_MODE_REQUEST: return g_holding.mode_request;
case HOLDING_HEADING_SETPOINT_X100: return (uint16_t)g_holding.heading_setpoint_x100;
case HOLDING_BRIGHTNESS_PCT: return g_holding.brightness_pct;
case HOLDING_ALARM_VOLUME_PCT: return g_holding.alarm_volume_pct;
case HOLDING_DODGE_OFFSET_DEG_X100: return (uint16_t)g_holding.dodge_offset_deg_x100;
default: return 0;
}
}
// Returns Modbus exception code (0 = ok). Side effect: stores value.
Modbus::Error write_holding(uint16_t addr, uint16_t value) {
switch (addr) {
case HOLDING_MODE_REQUEST:
if (value > 4) return Modbus::Error::ILLEGAL_DATA_VALUE;
g_holding.mode_request = value;
modes::request_mode((modes::Mode)value);
return Modbus::Error::SUCCESS;
case HOLDING_HEADING_SETPOINT_X100:
g_holding.heading_setpoint_x100 = (int16_t)value;
return Modbus::Error::SUCCESS;
case HOLDING_BRIGHTNESS_PCT:
if (value > 100) return Modbus::Error::ILLEGAL_DATA_VALUE;
g_holding.brightness_pct = value;
return Modbus::Error::SUCCESS;
case HOLDING_ALARM_VOLUME_PCT:
if (value > 100) return Modbus::Error::ILLEGAL_DATA_VALUE;
g_holding.alarm_volume_pct = value;
return Modbus::Error::SUCCESS;
case HOLDING_DODGE_OFFSET_DEG_X100:
g_holding.dodge_offset_deg_x100 = (int16_t)value;
return Modbus::Error::SUCCESS;
default:
return Modbus::Error::ILLEGAL_DATA_ADDRESS;
}
}
Modbus::Error write_coil(uint16_t addr, bool value) {
switch (addr) {
case COIL_CMD_ENGAGE_REQUEST:
g_coils.engage_request = value;
// Sprint 1: requesting engagement does nothing yet -- modes
// engine is implemented in Sprint 3+. Just log and store.
if (value) {
AR_LOGI(TAG, "engage request received (no-op in Sprint 1)");
}
return Modbus::Error::SUCCESS;
case COIL_CMD_DISENGAGE_REQUEST:
g_coils.disengage_request = value;
if (value) {
modes::force_standby("modbus-disengage");
}
return Modbus::Error::SUCCESS;
case COIL_CMD_ACK_ALL_ALARMS:
g_coils.ack_all = value;
if (value) {
AR_LOGI(TAG, "ack-all-alarms received (no alarms in Sprint 1)");
}
return Modbus::Error::SUCCESS;
case COIL_CMD_KNOB_ARM:
g_coils.knob_arm = value;
return Modbus::Error::SUCCESS;
default:
return Modbus::Error::ILLEGAL_DATA_ADDRESS;
}
}
// ----- eModbus worker callbacks ---------------------------------------------
ModbusMessage on_read_input(ModbusMessage req) {
uint16_t start, count;
req.get(2, start);
req.get(4, count);
if (count == 0 ||
(uint32_t)start + count > (uint32_t)INPUT_MAX_ADDR + 1U ||
count > 125) {
++g_err_count;
ModbusMessage resp;
resp.setError(req.getServerID(), req.getFunctionCode(),
Modbus::Error::ILLEGAL_DATA_VALUE);
return resp;
}
ModbusMessage resp;
resp.add(req.getServerID(), req.getFunctionCode(),
(uint8_t)(count * 2));
for (uint16_t i = 0; i < count; ++i) {
resp.add(read_input_register(start + i));
}
++g_req_count;
return resp;
}
ModbusMessage on_read_discrete(ModbusMessage req) {
uint16_t start, count;
req.get(2, start);
req.get(4, count);
if (count == 0 ||
(uint32_t)start + count > (uint32_t)DISCRETE_MAX_ADDR + 1U ||
count > 2000) {
++g_err_count;
ModbusMessage resp;
resp.setError(req.getServerID(), req.getFunctionCode(),
Modbus::Error::ILLEGAL_DATA_VALUE);
return resp;
}
ModbusMessage resp;
uint8_t byte_count = (uint8_t)((count + 7) / 8);
resp.add(req.getServerID(), req.getFunctionCode(), byte_count);
for (uint8_t b = 0; b < byte_count; ++b) {
uint8_t v = 0;
for (uint8_t bit = 0; bit < 8; ++bit) {
uint16_t idx = b * 8U + bit;
if (idx < count && read_discrete(start + idx)) {
v |= (uint8_t)(1U << bit);
}
}
resp.add(v);
}
++g_req_count;
return resp;
}
ModbusMessage on_read_holding(ModbusMessage req) {
uint16_t start, count;
req.get(2, start);
req.get(4, count);
if (count == 0 ||
(uint32_t)start + count > (uint32_t)HOLDING_MAX_ADDR + 1U ||
count > 125) {
++g_err_count;
ModbusMessage resp;
resp.setError(req.getServerID(), req.getFunctionCode(),
Modbus::Error::ILLEGAL_DATA_VALUE);
return resp;
}
ModbusMessage resp;
resp.add(req.getServerID(), req.getFunctionCode(),
(uint8_t)(count * 2));
for (uint16_t i = 0; i < count; ++i) {
resp.add(read_holding(start + i));
}
++g_req_count;
return resp;
}
ModbusMessage on_write_holding(ModbusMessage req) {
uint16_t addr, value;
req.get(2, addr);
req.get(4, value);
auto err = write_holding(addr, value);
if (err != Modbus::Error::SUCCESS) {
++g_err_count;
ModbusMessage resp;
resp.setError(req.getServerID(), req.getFunctionCode(), err);
return resp;
}
// Echo per Modbus 0x06 convention.
ModbusMessage resp;
resp.add(req.getServerID(), req.getFunctionCode(), addr, value);
++g_req_count;
return resp;
}
ModbusMessage on_write_coil(ModbusMessage req) {
uint16_t addr, value;
req.get(2, addr);
req.get(4, value);
// 0xFF00 = ON, 0x0000 = OFF per Modbus spec.
if (value != 0x0000 && value != 0xFF00) {
++g_err_count;
ModbusMessage resp;
resp.setError(req.getServerID(), req.getFunctionCode(),
Modbus::Error::ILLEGAL_DATA_VALUE);
return resp;
}
auto err = write_coil(addr, value == 0xFF00);
if (err != Modbus::Error::SUCCESS) {
++g_err_count;
ModbusMessage resp;
resp.setError(req.getServerID(), req.getFunctionCode(), err);
return resp;
}
ModbusMessage resp;
resp.add(req.getServerID(), req.getFunctionCode(), addr, value);
++g_req_count;
return resp;
}
} // namespace
void modbus_slave_init() {
// Register worker callbacks BEFORE starting the server (eModbus
// requirement).
g_server.registerWorker(SLAVE_ID, READ_INPUT_REGISTER, &on_read_input);
g_server.registerWorker(SLAVE_ID, READ_DISCR_INPUT, &on_read_discrete);
g_server.registerWorker(SLAVE_ID, READ_HOLD_REGISTER, &on_read_holding);
g_server.registerWorker(SLAVE_ID, WRITE_HOLD_REGISTER, &on_write_holding);
g_server.registerWorker(SLAVE_ID, WRITE_COIL, &on_write_coil);
AR_LOGI(TAG,
"modbus_slave_init: slave_id=%u inputs=%u discretes=%u "
"holdings=%u coils=%u",
(unsigned)SLAVE_ID, (unsigned)INPUT_COUNT, (unsigned)DISCRETE_COUNT,
(unsigned)HOLDING_COUNT, (unsigned)COIL_COUNT);
}
void modbus_slave_start() {
// UART2 on the AR-NMEA-IO is wired to RS-485.
Serial2.begin(BAUDRATE, SERIAL_8N1, PIN_RS485_RX, PIN_RS485_TX);
g_server.begin(Serial2, AR_TASK_CORE_COMMS);
g_running = true;
AR_LOGI(TAG, "modbus_slave_start: listening on UART2 @ %u baud (RX=%d TX=%d DE=%d)",
(unsigned)BAUDRATE, PIN_RS485_RX, PIN_RS485_TX, PIN_RS485_DE);
}
bool modbus_slave_is_running() { return g_running; }
uint32_t modbus_slave_request_count() { return g_req_count; }
uint32_t modbus_slave_error_count() { return g_err_count; }
} // namespace arautopilot::protocols::modbus
@@ -0,0 +1,45 @@
// =============================================================================
// modbus_slave.h -- Modbus RTU server (slave) interface
// =============================================================================
//
// Sprint 1: exposes the read-only telemetry registers (input registers and
// discrete inputs) and accepts writes to the holding registers and coils
// defined in modbus_registers.h (auto-generated).
//
// Reads come straight from the live telemetry helpers
// (modes::current_mode(), hal::rudder_sensor_latest(), etc.).
//
// Writes are validated and routed to the corresponding command handler
// (mode change, alarm ack, etc.). Invalid values are rejected with
// ILLEGAL_DATA_VALUE per Modbus convention.
//
// All Modbus internals (RX task, response framing, RS-485 DE/RE control)
// are delegated to the eModbus library, which spawns its own tasks on
// Core 0.
// =============================================================================
#pragma once
#include <cstdint>
namespace arautopilot::protocols::modbus {
/// Initialise the RS-485 UART, configure the Modbus server, and register
/// every read/write callback. Must be called from setup() after di_init()
/// and rudder_sensor_init().
void modbus_slave_init();
/// Start the eModbus server. After this returns, the slave is listening on
/// the configured UART/baudrate and replies asynchronously.
void modbus_slave_start();
/// True after modbus_slave_start() has successfully initialised the server.
bool modbus_slave_is_running();
/// Number of valid requests processed since boot (cheap performance counter).
uint32_t modbus_slave_request_count();
/// Number of malformed requests / illegal-data-value rejections since boot.
uint32_t modbus_slave_error_count();
} // namespace arautopilot::protocols::modbus
@@ -0,0 +1,178 @@
// =============================================================================
// nmea2000_consumer.cpp -- NMEA 2000 backbone consumer
// =============================================================================
#include "nmea2000_consumer.h"
#include <Arduino.h>
// Override the default ESP32 CAN pins (16/4) to match our AR-NMEA-IO board.
#include "../hal/pinout.h"
#define ESP32_CAN_TX_PIN ((gpio_num_t)PIN_CAN_TX)
#define ESP32_CAN_RX_PIN ((gpio_num_t)PIN_CAN_RX)
#include <NMEA2000_CAN.h>
#include <N2kMessages.h>
#include "../system/ar_log.h"
#include "../system/task_config.h"
namespace arautopilot::protocols::nmea2000 {
namespace {
constexpr const char* TAG = "AR/N2K";
constexpr uint32_t STALE_THRESHOLD_MS = 5000;
portMUX_TYPE g_mux = portMUX_INITIALIZER_UNLOCKED;
HeadingSnapshot g_snap{
.heading_deg = 0.0f,
.is_true = false,
.rate_of_turn_dps = 0.0f,
.heading_age_ms = 0,
.rot_age_ms = 0,
.heading_valid = false,
.rot_valid = false,
};
float rad_to_deg_pos(float rad) {
float d = rad * (180.0f / (float)M_PI);
// Normalise to 0..360.
while (d < 0.0f) d += 360.0f;
while (d >= 360.0f) d -= 360.0f;
return d;
}
float rad_to_deg_signed(float rad) {
return rad * (180.0f / (float)M_PI);
}
void HandleHeading(const tN2kMsg& msg) {
unsigned char sid;
double heading = 0.0, deviation = 0.0, variation = 0.0;
tN2kHeadingReference ref = N2khr_Unavailable;
if (!ParseN2kHeading(msg, sid, heading, deviation, variation, ref)) {
return;
}
if (heading > 1e8) {
// N2k "unavailable" markers come through as huge doubles.
return;
}
const float heading_deg = rad_to_deg_pos((float)heading);
const bool is_true = (ref == N2khr_true);
const uint32_t now = millis();
portENTER_CRITICAL(&g_mux);
g_snap.heading_deg = heading_deg;
g_snap.is_true = is_true;
g_snap.heading_age_ms = now;
g_snap.heading_valid = true;
portEXIT_CRITICAL(&g_mux);
AR_LOGV(TAG, "PGN 127250 heading=%.2f deg (%s)", heading_deg,
is_true ? "true" : "magnetic");
}
void HandleROT(const tN2kMsg& msg) {
unsigned char sid;
double rot = 0.0;
if (!ParseN2kRateOfTurn(msg, sid, rot)) {
return;
}
if (rot > 1e8 || rot < -1e8) {
return;
}
const float rot_dps = rad_to_deg_signed((float)rot);
const uint32_t now = millis();
portENTER_CRITICAL(&g_mux);
g_snap.rate_of_turn_dps = rot_dps;
g_snap.rot_age_ms = now;
g_snap.rot_valid = true;
portEXIT_CRITICAL(&g_mux);
AR_LOGV(TAG, "PGN 127251 ROT=%.3f deg/s", rot_dps);
}
// One global dispatcher because NMEA2000.SetMsgHandler() takes a single
// callback that we have to filter by PGN ourselves.
void MessageHandler(const tN2kMsg& msg) {
switch (msg.PGN) {
case 127250L:
HandleHeading(msg);
break;
case 127251L:
HandleROT(msg);
break;
default:
// Sprint 1: ignore everything else.
break;
}
}
void RxTask(void* /*pv*/) {
AR_LOGI(TAG, "nmea2000_consumer task started on core %d", xPortGetCoreID());
for (;;) {
NMEA2000.ParseMessages();
// Update validity flags based on age.
const uint32_t now = millis();
portENTER_CRITICAL(&g_mux);
if (g_snap.heading_valid && (now - g_snap.heading_age_ms) > STALE_THRESHOLD_MS) {
g_snap.heading_valid = false;
}
if (g_snap.rot_valid && (now - g_snap.rot_age_ms) > STALE_THRESHOLD_MS) {
g_snap.rot_valid = false;
}
portEXIT_CRITICAL(&g_mux);
// 100 Hz polling is plenty -- the CAN driver buffers incoming frames.
vTaskDelay(pdMS_TO_TICKS(10));
}
}
} // namespace
void nmea2000_consumer_init() {
NMEA2000.SetProductInformation(
"AR-AP-1", // Manufacturer's Model serial code
100, // Manufacturer's product code
"AR-Autopilot Controller v1", // Model ID
AR_FW_VERSION, // SW version
"AR-NMEA-IO v1.0" // Model version
);
NMEA2000.SetDeviceInformation(
1, // Unique number
150, // Device function: Autopilot
40, // Device class: Steering and Control surfaces
2046 // Manufacturer code: reserved/test (real one needs NMEA registration)
);
NMEA2000.SetMode(tNMEA2000::N2km_ListenAndNode, 25);
NMEA2000.EnableForward(false);
NMEA2000.SetMsgHandler(&MessageHandler);
if (NMEA2000.Open()) {
AR_LOGI(TAG,
"nmea2000_consumer_init: stack open, CAN TX=%d RX=%d, "
"subscribed to PGN 127250 + 127251",
PIN_CAN_TX, PIN_CAN_RX);
} else {
AR_LOGE(TAG,
"nmea2000_consumer_init: NMEA2000.Open() failed (CAN driver "
"init error). System will continue but no N2K traffic.");
}
}
void nmea2000_consumer_start_task() {
xTaskCreatePinnedToCore(RxTask, "n2k_rx", AR_TASK_STACK_N2K_RX, nullptr,
AR_TASK_PRIO_N2K_RX, nullptr, AR_TASK_CORE_COMMS);
}
HeadingSnapshot nmea2000_latest() {
HeadingSnapshot copy;
portENTER_CRITICAL(&g_mux);
copy = g_snap;
portEXIT_CRITICAL(&g_mux);
return copy;
}
bool nmea2000_is_stale() {
const auto s = nmea2000_latest();
return !s.heading_valid;
}
} // namespace arautopilot::protocols::nmea2000
@@ -0,0 +1,46 @@
// =============================================================================
// nmea2000_consumer.h -- NMEA 2000 backbone consumer
// =============================================================================
//
// Sprint 1 subscribes to PGN 127250 (Vessel Heading) and PGN 127251
// (Rate of Turn) from the boat's NMEA 2000 backbone. The latest values
// are stashed in a thread-safe snapshot that the Modbus slave (and later
// the PID outer loop) read from.
//
// Later sprints will also subscribe to PGN 129025/129029 (Position),
// 129026 (COG/SOG), 129284 (Navigation Data), 127257 (Attitude).
//
// This module owns the NMEA2000 instance and its dedicated FreeRTOS task
// pinned to Core 0.
// =============================================================================
#pragma once
#include <cstdint>
namespace arautopilot::protocols::nmea2000 {
struct HeadingSnapshot {
float heading_deg; ///< 0..360, magnetic or true depending on source
bool is_true; ///< true if reference is "true north", false if magnetic
float rate_of_turn_dps; ///< signed deg/s; positive = turning to starboard
uint32_t heading_age_ms; ///< millis() at the last 127250 update
uint32_t rot_age_ms; ///< millis() at the last 127251 update
bool heading_valid; ///< true if the heading is fresh (<5 s old)
bool rot_valid; ///< true if the ROT is fresh (<5 s old)
};
/// Initialise the NMEA2000 stack with our PGN handlers.
void nmea2000_consumer_init();
/// Spawn the FreeRTOS task that pumps NMEA2000.ParseMessages() forever.
void nmea2000_consumer_start_task();
/// Thread-safe read of the latest heading + ROT snapshot.
HeadingSnapshot nmea2000_latest();
/// True if either heading_age_ms or rot_age_ms exceeds the stale-threshold
/// (default 5 s, brief section 7).
bool nmea2000_is_stale();
} // namespace arautopilot::protocols::nmea2000
@@ -0,0 +1,77 @@
// =============================================================================
// safety/safety_monitor.cpp -- 50 Hz safety task
// =============================================================================
#include "safety_monitor.h"
#include <Arduino.h>
#include "../hal/di_do.h"
#include "../hal/pinout.h"
#include "../hal/rudder_actuator.h"
#include "../modes/standby.h"
#include "../system/ar_log.h"
#include "../system/task_config.h"
#include "watchdog.h"
namespace arautopilot::safety {
namespace {
constexpr const char* TAG = "AR/SAFE";
void SafetyTask(void* /*pv*/) {
AR_LOGI(TAG, "safety_monitor task started on core %d (50 Hz)",
xPortGetCoreID());
// Subscribe to the watchdog. Every loop iteration feeds it; if this
// task ever stops looping the chip resets to STANDBY on boot.
watchdog_subscribe_current_task();
TickType_t last_wake = xTaskGetTickCount();
for (;;) {
hal::di_poll();
// ---- DI1: Engage/Disengage physical button -----------------------
// The brief specifies this button "ALWAYS DISENGAGES" -- pressing
// it must put the system in STANDBY no matter what mode we're in.
// We trigger on the rising edge so a held button doesn't keep
// spamming the log.
if (hal::di_rising_edge(PIN_DI1_DISENGAGE_BUTTON)) {
modes::force_standby("DI1 physical button");
hal::rudder_actuator_power_off();
}
// ---- DI4: External critical alarm (VMS blackout / genset) --------
if (hal::di_rising_edge(PIN_DI4_EXTERNAL_ALARM)) {
modes::force_standby("DI4 external alarm");
hal::rudder_actuator_power_off();
}
// ---- Limit switches: cut power if rudder hit a mechanical stop --
// Even though rudder_command() refuses to drive into a limit, a
// hardware failure could still command the wrong direction. As an
// extra interlock, if BOTH limits assert at once we cut master
// power -- something is seriously wrong with the feedback wiring.
if (hal::di_read(PIN_DI2_LIMIT_SWITCH_PORT) &&
hal::di_read(PIN_DI3_LIMIT_SWITCH_STBD)) {
AR_LOGE(TAG,
"both limit switches asserted simultaneously -- cutting "
"actuator power (wiring fault?)");
hal::rudder_actuator_power_off();
}
watchdog_feed();
vTaskDelayUntil(&last_wake, pdMS_TO_TICKS(AR_PERIOD_MS_SAFETY));
}
}
} // namespace
void safety_monitor_start_task() {
xTaskCreatePinnedToCore(SafetyTask, "safety_monitor",
AR_TASK_STACK_SAFETY, nullptr,
AR_TASK_PRIO_SAFETY, nullptr,
AR_TASK_CORE_REALTIME);
}
} // namespace arautopilot::safety
@@ -0,0 +1,26 @@
// =============================================================================
// safety/safety_monitor.h -- safety monitor task
// =============================================================================
//
// 50 Hz task on Core 1 that:
// - Polls every DI through hal::di_poll().
// - Reacts to PIN_DI1_DISENGAGE_BUTTON rising edge: forces STANDBY,
// kills actuator power.
// - Reacts to limit switches: cuts actuator power if the rudder is
// trying to drive into a limit.
// - Reacts to PIN_DI4_EXTERNAL_ALARM (VMS critical): forces STANDBY.
// - Subscribes itself to the TWDT and feeds it every loop iteration.
//
// Sprint 1: limited to the above. Sprint 6 expands this with the full
// alarm catalogue (off-course, rudder not responding, etc.).
// =============================================================================
#pragma once
namespace arautopilot::safety {
/// Spawn the safety monitor task. Must be called AFTER di_init() and
/// rudder_actuator_init().
void safety_monitor_start_task();
} // namespace arautopilot::safety
@@ -0,0 +1,40 @@
// =============================================================================
// safety/watchdog.cpp -- TWDT setup + helpers
// =============================================================================
#include "watchdog.h"
#include <Arduino.h>
#include <esp_task_wdt.h>
#include "../system/ar_log.h"
#include "../system/task_config.h"
namespace arautopilot::safety {
namespace {
constexpr const char* TAG = "AR/SAFE";
} // namespace
void watchdog_init() {
// ESP-IDF 5.x: esp_task_wdt_init takes a config struct, but
// esp32 Arduino core wraps it with a simpler signature.
esp_err_t err = esp_task_wdt_init(AR_WATCHDOG_TIMEOUT_S, true);
if (err != ESP_OK) {
AR_LOGE(TAG, "esp_task_wdt_init failed: %d", (int)err);
return;
}
AR_LOGI(TAG, "watchdog_init: TWDT timeout %ds, panic on expire",
AR_WATCHDOG_TIMEOUT_S);
}
void watchdog_subscribe_current_task() {
esp_err_t err = esp_task_wdt_add(nullptr);
if (err != ESP_OK && err != ESP_ERR_INVALID_ARG) {
AR_LOGW(TAG, "esp_task_wdt_add failed: %d", (int)err);
}
}
void watchdog_feed() { esp_task_wdt_reset(); }
} // namespace arautopilot::safety
@@ -0,0 +1,29 @@
// =============================================================================
// safety/watchdog.h -- Task Watchdog Timer (TWDT)
// =============================================================================
//
// Hooks the ESP32 task watchdog so that if the real-time control tasks
// (PID inner, PID outer, safety monitor) ever fail to feed the watchdog
// within AR_WATCHDOG_TIMEOUT_S, the chip resets and reboots cleanly to
// STANDBY mode.
//
// Brief section 7: "El ESP32 reinicia automaticamente si el firmware se
// cuelga >2 segundos. Al reiniciar: Estado del piloto pasa a STANDBY."
// =============================================================================
#pragma once
namespace arautopilot::safety {
/// Configure and start the Task Watchdog Timer. Tasks that want to be
/// monitored must call watchdog_subscribe_current_task() once and then
/// watchdog_feed() at least once per AR_WATCHDOG_TIMEOUT_S.
void watchdog_init();
/// Add the current task to the watchdog's monitored set.
void watchdog_subscribe_current_task();
/// Feed the watchdog from the current task.
void watchdog_feed();
} // namespace arautopilot::safety
@@ -0,0 +1,35 @@
// =============================================================================
// ar_log.h -- AR-Autopilot logging facade
// =============================================================================
//
// Thin wrapper around the ESP32 Arduino log_X / ESP_LOGX macros so that the
// rest of the firmware uses one consistent style. Compile-time level is
// controlled by CORE_DEBUG_LEVEL in platformio.ini.
//
// Levels (matching ARDUHAL_LOG_LEVEL_*):
// 0 NONE
// 1 ERROR
// 2 WARN
// 3 INFO <- default in release
// 4 DEBUG
// 5 VERBOSE <- default in debug
// =============================================================================
#pragma once
#include <Arduino.h>
// Tag prefix conventions used across the codebase:
// "AR/MAIN" -- main.cpp boot/shutdown
// "AR/PID" -- PID loops
// "AR/HAL" -- hardware abstraction
// "AR/MB" -- Modbus slave
// "AR/N2K" -- NMEA 2000 consumer
// "AR/SAFE" -- safety / watchdog / disengage
// "AR/SYS" -- health / lifecycle / metrics
#define AR_LOGE(tag, fmt, ...) log_e("[%s] " fmt, tag, ##__VA_ARGS__)
#define AR_LOGW(tag, fmt, ...) log_w("[%s] " fmt, tag, ##__VA_ARGS__)
#define AR_LOGI(tag, fmt, ...) log_i("[%s] " fmt, tag, ##__VA_ARGS__)
#define AR_LOGD(tag, fmt, ...) log_d("[%s] " fmt, tag, ##__VA_ARGS__)
#define AR_LOGV(tag, fmt, ...) log_v("[%s] " fmt, tag, ##__VA_ARGS__)
@@ -0,0 +1,50 @@
// =============================================================================
// heartbeat.cpp -- LED + uptime heartbeat task
// =============================================================================
//
// Blinks PIN_DO5_ENGAGED_LAMP at 1 Hz to give a visible "the firmware is
// alive" signal at the bench. In Sprint 1 we co-opt this LED because there
// is no pilot to engage yet; from Sprint 6 onwards the engaged lamp will be
// driven by the actual pilot state and the heartbeat will move to an
// internal counter only.
//
// Also logs uptime + free heap once per second so a terminal observer can
// see the system is healthy.
// =============================================================================
#include <Arduino.h>
#include "../hal/pinout.h"
#include "ar_log.h"
#include "task_config.h"
namespace {
constexpr const char* TAG = "AR/SYS";
} // namespace
static void HeartbeatTask(void* /*pv*/) {
pinMode(PIN_DO5_ENGAGED_LAMP, OUTPUT);
bool led_on = false;
uint32_t tick = 0;
AR_LOGI(TAG, "heartbeat task started on core %d, pin %d", xPortGetCoreID(),
PIN_DO5_ENGAGED_LAMP);
TickType_t last_wake = xTaskGetTickCount();
for (;;) {
led_on = !led_on;
digitalWrite(PIN_DO5_ENGAGED_LAMP, led_on ? HIGH : LOW);
AR_LOGD(TAG, "tick=%u uptime=%lus free_heap=%u min_free=%u", tick,
millis() / 1000U, ESP.getFreeHeap(), ESP.getMinFreeHeap());
++tick;
vTaskDelayUntil(&last_wake, pdMS_TO_TICKS(AR_PERIOD_MS_HEARTBEAT));
}
}
void ar_start_heartbeat_task() {
xTaskCreatePinnedToCore(HeartbeatTask, "heartbeat", AR_TASK_STACK_HEARTBEAT,
nullptr, AR_TASK_PRIO_HEARTBEAT, nullptr,
AR_TASK_CORE_COMMS);
}
@@ -0,0 +1,68 @@
// =============================================================================
// task_config.h -- FreeRTOS task layout for AR-Autopilot
// =============================================================================
//
// Single source of truth for stack sizes, priorities, and core pinning of
// every long-running task in the firmware. Centralising this here makes the
// real-time profile of the system reviewable at a glance.
//
// Pinning policy (brief section 6, rule #11 -- "deterministic latency"):
//
// Core 1 (APP_CPU) -- safety-critical real-time:
// AR_TASK_CORE_REALTIME = 1
// - PID inner loop (Sprint 2; stub in Sprint 1)
// - PID outer loop (Sprint 3; stub in Sprint 1)
// - Rudder sensor (Sprint 1: 100 Hz median filter)
// - Safety monitor (Sprint 1: limit switches, watchdog feed)
//
// Core 0 (PRO_CPU) -- communications + housekeeping:
// AR_TASK_CORE_COMMS = 0
// - NMEA 2000 RX (Sprint 1: PGN 127250 / 127251)
// - Modbus slave (Sprint 1: eModbus internals already async)
// - Health reporter (Sprint 1: 1 Hz log)
//
// This split guarantees the real-time control loops cannot be starved or
// jittered by bus traffic, even if NMEA 2000 saturates or the Modbus client
// bursts.
//
// Priorities use the standard ESP32 FreeRTOS scale (0 idle .. 24 max).
// configMAX_PRIORITIES is 25 on default ESP32 Arduino builds.
// =============================================================================
#pragma once
// Core assignment
#define AR_TASK_CORE_REALTIME 1
#define AR_TASK_CORE_COMMS 0
// Priorities (higher = more priority)
#define AR_TASK_PRIO_PID_INNER 24 // hard real-time, 50 Hz
#define AR_TASK_PRIO_RUDDER_SENSOR 23 // 100 Hz ADC, must feed PID fresh data
#define AR_TASK_PRIO_PID_OUTER 22 // 10 Hz heading control
#define AR_TASK_PRIO_SAFETY 21 // limit switches, watchdog feed
#define AR_TASK_PRIO_N2K_RX 15 // CAN polling, event-driven
#define AR_TASK_PRIO_MODBUS 14 // eModbus internal tasks (delegated)
#define AR_TASK_PRIO_HEARTBEAT 10 // LED blink + uptime log
#define AR_TASK_PRIO_HEALTH 5 // periodic stats, low priority
// Stack sizes (bytes). Tune these once we see real high-water marks via
// uxTaskGetStackHighWaterMark() in the health reporter.
#define AR_TASK_STACK_PID_INNER 4096
#define AR_TASK_STACK_PID_OUTER 4096
#define AR_TASK_STACK_RUDDER_SENSOR 3072
#define AR_TASK_STACK_SAFETY 3072
#define AR_TASK_STACK_N2K_RX 6144 // NMEA2000 parsing is heap-heavy
#define AR_TASK_STACK_MODBUS 4096
#define AR_TASK_STACK_HEARTBEAT 2048
#define AR_TASK_STACK_HEALTH 3072
// Loop periods (ms). Convert with pdMS_TO_TICKS() at the use site.
#define AR_PERIOD_MS_PID_INNER 20 // 50 Hz
#define AR_PERIOD_MS_PID_OUTER 100 // 10 Hz
#define AR_PERIOD_MS_RUDDER_SENSOR 10 // 100 Hz
#define AR_PERIOD_MS_SAFETY 20 // 50 Hz
#define AR_PERIOD_MS_HEARTBEAT 1000 // 1 Hz LED blink
#define AR_PERIOD_MS_HEALTH 5000 // every 5 s
// Watchdog (brief section 7)
#define AR_WATCHDOG_TIMEOUT_S 2