Add src/mpu6000.c implementing a complementary filter (α=0.98) on top of the existing icm42688 SPI driver. Fixes wrong scale factors in balance.c (was ±250°/s / ±2g; hardware is configured ±2000°/s / ±16g). Fusion now lives in the IMU driver layer; balance_update() consumes IMUData directly. - mpu6000_init(): calls icm42688_init(), seeds filter state - mpu6000_read(): reads raw SPI, applies complementary filter, returns fused pitch (degrees) + pitch_rate (°/s) + accel_x/z (g) - balance.c: removes duplicated fusion code, uses IMUData.pitch - main.c: switches to mpu6000_init()/mpu6000_read(), updates telemetry Co-Authored-By: Claude Sonnet 4.6 <noreply@anthropic.com>
86 lines
2.6 KiB
C
86 lines
2.6 KiB
C
/*
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* mpu6000.c — IMU Sensor Fusion for MPU6000
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*
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* Wraps the icm42688 SPI driver (which auto-detects MPU6000) and applies
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* a complementary filter to produce a stable pitch estimate.
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*
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* Hardware: MAMBA F722S, MPU6000 on SPI1, CW270 alignment
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* Config: Gyro ±2000°/s (init_mpu6000 sets FS_SEL=3)
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* Accel ±16g (init_mpu6000 sets AFS_SEL=3)
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*/
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#include "mpu6000.h"
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#include "icm42688.h"
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#include "stm32f7xx_hal.h"
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#include <math.h>
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/* Scale factors matching init_mpu6000() config in icm42688.c */
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#define GYRO_SCALE (1.0f / 16.384f) /* LSB to °/s — ±2000°/s range */
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#define ACCEL_SCALE (1.0f / 2048.0f) /* LSB to g — ±16g range */
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/*
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* Complementary filter coefficient.
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* 0.98 = trust gyro integration, 0.02 = accel correction for drift.
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* Tune higher (0.99) for noisier environments.
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*/
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#define COMP_ALPHA 0.98f
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/* Filter state */
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static float s_pitch = 0.0f;
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static uint32_t s_last_tick = 0;
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bool mpu6000_init(void) {
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int ret = icm42688_init();
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if (ret == 0) {
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s_pitch = 0.0f;
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s_last_tick = HAL_GetTick();
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}
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return (ret == 0);
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}
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void mpu6000_read(IMUData *data) {
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icm42688_data_t raw;
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icm42688_read(&raw);
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/* Compute dt from wall clock — robust to loop jitter */
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uint32_t now = HAL_GetTick();
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uint32_t elapsed_ms = now - s_last_tick;
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if (elapsed_ms == 0) elapsed_ms = 1; /* min 1ms to avoid divide-by-zero */
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if (elapsed_ms > 100) elapsed_ms = 100; /* clamp: don't integrate stale data */
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float dt = elapsed_ms * 0.001f;
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s_last_tick = now;
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/* Convert raw to physical units */
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float ax = raw.ax * ACCEL_SCALE; /* g */
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float az = raw.az * ACCEL_SCALE; /* g */
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/*
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* Gyro pitch axis with CW270 alignment: pitch rate = gx.
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* Sign may need inverting depending on mounting orientation —
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* verify during bench test (positive nose-up should be positive).
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*/
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float gyro_pitch_rate = raw.gx * GYRO_SCALE; /* °/s */
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/*
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* Accel pitch angle (degrees).
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* CW270 alignment: pitch = atan2(ax, az).
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* Valid while ax² + az² ≈ 1g (i.e., low linear acceleration).
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*/
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float accel_pitch = atan2f(ax, az) * (180.0f / 3.14159265358979f);
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/*
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* Complementary filter:
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* pitch = α * (pitch + ω*dt) + (1−α) * accel_pitch
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*
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* Gyro integration tracks fast dynamics; accel correction
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* prevents long-term drift.
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*/
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s_pitch = COMP_ALPHA * (s_pitch + gyro_pitch_rate * dt)
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+ (1.0f - COMP_ALPHA) * accel_pitch;
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data->pitch = s_pitch;
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data->pitch_rate = gyro_pitch_rate;
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data->accel_x = ax;
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data->accel_z = az;
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}
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