mirror of https://github.com/ArduPilot/ardupilot
SITL: use new HIL compass API
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@ -54,7 +54,7 @@ private:
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// these methods are static as they are called
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// from the timer
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static void _update_barometer(float height);
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static void _update_compass(float roll, float pitch, float yaw);
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static void _update_compass(float rollDeg, float pitchDeg, float yawDeg);
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struct gps_data {
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double latitude;
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@ -89,7 +89,6 @@ private:
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static float _gyro_drift(void);
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static float _rand_float(void);
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static Vector3f _rand_vec3f(void);
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static Vector3f _heading_to_mag(float roll, float pitch, float yaw);
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// signal handlers
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static void _sig_fpe(int signum);
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@ -21,60 +21,21 @@
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using namespace AVR_SITL;
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#define MAG_OFS_X 5.0
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#define MAG_OFS_Y 13.0
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#define MAG_OFS_Z -18.0
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// inclination in Canberra (degrees)
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#define MAG_INCLINATION -66
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// magnetic field strength in Canberra as observed
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// using an APM1 with 5883L compass
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#define MAG_FIELD_STRENGTH 818
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/*
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given a magnetic heading, and roll, pitch, yaw values,
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calculate consistent magnetometer components
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All angles are in radians
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*/
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Vector3f SITL_State::_heading_to_mag(float roll, float pitch, float yaw)
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{
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Vector3f Bearth, m;
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Matrix3f R;
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float declination = AP_Declination::get_declination(_sitl->state.latitude, _sitl->state.longitude);
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// Bearth is the magnetic field in Canberra. We need to adjust
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// it for inclination and declination
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Bearth(MAG_FIELD_STRENGTH, 0, 0);
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R.from_euler(0, -ToRad(MAG_INCLINATION), ToRad(declination));
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Bearth = R * Bearth;
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// create a rotation matrix for the given attitude
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R.from_euler(roll, pitch, yaw);
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// convert the earth frame magnetic vector to body frame, and
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// apply the offsets
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m = R.transposed() * Bearth - Vector3f(MAG_OFS_X, MAG_OFS_Y, MAG_OFS_Z);
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return m + (_rand_vec3f() * _sitl->mag_noise);
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}
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/*
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setup the compass with new input
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all inputs are in degrees
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*/
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void SITL_State::_update_compass(float roll, float pitch, float yaw)
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void SITL_State::_update_compass(float rollDeg, float pitchDeg, float yawDeg)
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{
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if (_compass == NULL) {
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// no compass in this sketch
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return;
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}
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Vector3f m = _heading_to_mag(ToRad(roll),
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ToRad(pitch),
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ToRad(yaw));
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_compass->setHIL(m.x, m.y, m.z);
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_compass->setHIL(radians(rollDeg), radians(pitchDeg), radians(yawDeg));
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Vector3f noise = _rand_vec3f() * _sitl->mag_noise;
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_compass->mag_x += noise.x;
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_compass->mag_y += noise.y;
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_compass->mag_z += noise.z;
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}
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#endif
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