Files
air-mouse/source/imu.cpp
2026-03-01 21:35:36 +01:00

83 lines
3.7 KiB
C++

#include "imu.h"
#include "Wire.h"
#include <math.h>
LSM6DS3 imu(I2C_MODE, 0x6A);
float rollSin = 0.0f; // identity: no rotation
float rollCos = 1.0f;
// ─── I2C helpers ──────────────────────────────────────────────────────────────
void imuWriteReg(uint8_t reg, uint8_t val) {
// LSM6DS3 is on Wire1 (internal I2C, SDA=P0.17, SCL=P0.16), NOT Wire (external pins 4/5)
Wire1.beginTransmission(0x6A); Wire1.write(reg); Wire1.write(val); Wire1.endTransmission();
}
uint8_t imuReadReg(uint8_t reg) {
Wire1.beginTransmission(0x6A); Wire1.write(reg); Wire1.endTransmission(false);
Wire1.requestFrom((uint8_t)0x6A, (uint8_t)1);
return Wire1.available() ? Wire1.read() : 0;
}
// ─── Temperature ──────────────────────────────────────────────────────────────
float readIMUTemp() {
int16_t raw = (int16_t)((imuReadReg(REG_OUT_TEMP_H) << 8) | imuReadReg(REG_OUT_TEMP_L));
return 25.0f + (float)raw / 256.0f;
}
// ─── Calibration ──────────────────────────────────────────────────────────────
void calibrateGyroBias() {
Serial.println("[CAL] Hold still...");
double sx=0, sy=0, sz=0;
double sax=0, say=0;
for (int i=0; i<BIAS_SAMPLES; i++) {
sx += imu.readFloatGyroX(); sy += imu.readFloatGyroY(); sz += imu.readFloatGyroZ();
sax += imu.readFloatAccelX(); say += imu.readFloatAccelY();
digitalWrite(LED_GREEN, (i%20 < 10)); delay(5); // green flutter during calibration
}
biasGX = (float)(sx/BIAS_SAMPLES);
biasGY = (float)(sy/BIAS_SAMPLES);
biasGZ = (float)(sz/BIAS_SAMPLES);
calTempC = readIMUTemp();
angleX = angleY = accumX = accumY = 0.0f;
// Roll compensation: compute device yaw on the table from gravity's horizontal components.
// ax/ay are small when flat; their ratio gives the rotation angle θ.
// Firmware maps: screenX ← -gz, screenY ← -gy.
// With device rotated θ CW: screenX ← -(gz·cosθ + gy·sinθ), screenY ← -(gy·cosθ - gz·sinθ).
float ax_avg = (float)(sax / BIAS_SAMPLES);
float ay_avg = (float)(say / BIAS_SAMPLES);
float norm = sqrtf(ax_avg*ax_avg + ay_avg*ay_avg);
if (norm > 0.05f) { // only update if we can see meaningful tilt (>~3°)
rollSin = ax_avg / norm;
rollCos = -ay_avg / norm; // negative: gravity pulls in -Y when flat and nominal
} else {
rollSin = 0.0f;
rollCos = 1.0f;
}
Serial.print("[CAL] roll="); Serial.print(atan2f(rollSin, rollCos)*(180.f/PI), 1); Serial.println("deg");
#ifdef FEATURE_TELEMETRY
statRecalCount++;
float bxr = biasGX*(PI/180.f), byr = biasGY*(PI/180.f), bzr = biasGZ*(PI/180.f);
statBiasRms = sqrtf((bxr*bxr + byr*byr + bzr*bzr) / 3.0f);
#endif
digitalWrite(LED_GREEN, HIGH); // off after calibration
Serial.print("[CAL] T="); Serial.print(calTempC,1);
Serial.print("C bias="); Serial.print(biasGX,4);
Serial.print(","); Serial.print(biasGY,4);
Serial.print(","); Serial.println(biasGZ,4);
}
// ─── Motion curve ─────────────────────────────────────────────────────────────
float applyCurve(float v) {
switch (cfg.curve) {
case CURVE_SQUARE: return (v >= 0 ? 1.f : -1.f) * v * v;
case CURVE_SQRT: return (v >= 0 ? 1.f : -1.f) * sqrtf(fabsf(v));
default: return v;
}
}
float applyAcceleration(float d) { return d * (1.0f + fabsf(d) * cfg.accelStrength); }