void orientationCalcQuat_i(struct OrientationReps* orientation) {
if (bit_is_set(orientation->status, ORREP_QUAT_I))
return;
if (bit_is_set(orientation->status, ORREP_QUAT_F)) {
QUAT_BFP_OF_REAL(orientation->quat_i, orientation->quat_f);
}
else if (bit_is_set(orientation->status, ORREP_RMAT_I)) {
INT32_QUAT_OF_RMAT(orientation->quat_i, orientation->rmat_i);
}
else if (bit_is_set(orientation->status, ORREP_EULER_I)) {
INT32_QUAT_OF_EULERS(orientation->quat_i, orientation->eulers_i);
}
else if (bit_is_set(orientation->status, ORREP_RMAT_F)) {
RMAT_BFP_OF_REAL(orientation->rmat_i, orientation->rmat_f);
SetBit(orientation->status, ORREP_RMAT_I);
INT32_QUAT_OF_RMAT(orientation->quat_i, orientation->rmat_i);
}
else if (bit_is_set(orientation->status, ORREP_EULER_F)) {
EULERS_BFP_OF_REAL(orientation->eulers_i, orientation->eulers_f);
SetBit(orientation->status, ORREP_EULER_I);
INT32_QUAT_OF_EULERS(orientation->quat_i, orientation->eulers_i);
}
/* set bit to indicate this representation is computed */
SetBit(orientation->status, ORREP_QUAT_I);
}
void imu_init(void) {
/* initialises neutrals */
RATES_ASSIGN(imu.gyro_neutral, IMU_GYRO_P_NEUTRAL, IMU_GYRO_Q_NEUTRAL, IMU_GYRO_R_NEUTRAL);
VECT3_ASSIGN(imu.accel_neutral, IMU_ACCEL_X_NEUTRAL, IMU_ACCEL_Y_NEUTRAL, IMU_ACCEL_Z_NEUTRAL);
VECT3_ASSIGN(imu.mag_neutral, IMU_MAG_X_NEUTRAL, IMU_MAG_Y_NEUTRAL, IMU_MAG_Z_NEUTRAL);
/*
Compute quaternion and rotation matrix
for conversions between body and imu frame
*/
#if defined IMU_BODY_TO_IMU_PHI && defined IMU_BODY_TO_IMU_THETA & defined IMU_BODY_TO_IMU_PSI
struct Int32Eulers body_to_imu_eulers =
{ ANGLE_BFP_OF_REAL(IMU_BODY_TO_IMU_PHI),
ANGLE_BFP_OF_REAL(IMU_BODY_TO_IMU_THETA),
ANGLE_BFP_OF_REAL(IMU_BODY_TO_IMU_PSI) };
INT32_QUAT_OF_EULERS(imu.body_to_imu_quat, body_to_imu_eulers);
INT32_QUAT_NORMALISE(imu.body_to_imu_quat);
INT32_RMAT_OF_EULERS(imu.body_to_imu_rmat, body_to_imu_eulers);
#else
INT32_QUAT_ZERO(imu.body_to_imu_quat);
INT32_RMAT_ZERO(imu.body_to_imu_rmat);
#endif
imu_impl_init();
}
static void test_10(void) {
struct FloatEulers euler;
EULERS_ASSIGN(euler , RadOfDeg(0.), RadOfDeg(10.), RadOfDeg(0.));
DISPLAY_FLOAT_EULERS_DEG("euler", euler);
struct FloatQuat quat;
FLOAT_QUAT_OF_EULERS(quat, euler);
DISPLAY_FLOAT_QUAT("####quat", quat);
struct Int32Eulers euleri;
EULERS_BFP_OF_REAL(euleri, euler);
DISPLAY_INT32_EULERS("euleri", euleri);
struct Int32Quat quati;
INT32_QUAT_OF_EULERS(quati, euleri);
DISPLAY_INT32_QUAT("####quat", quati);
struct Int32RMat rmati;
INT32_RMAT_OF_EULERS(rmati, euleri);
DISPLAY_INT32_RMAT("####rmat", rmati);
struct Int32Quat quat_ltp_to_body;
struct Int32Quat body_to_imu_quat;
INT32_QUAT_ZERO( body_to_imu_quat);
INT32_QUAT_COMP_INV(quat_ltp_to_body, body_to_imu_quat, quati);
DISPLAY_INT32_QUAT("####quat_ltp_to_body", quat_ltp_to_body);
}
void imu_init(void) {
/* initialises neutrals */
RATES_ASSIGN(imu.gyro_neutral, IMU_GYRO_P_NEUTRAL, IMU_GYRO_Q_NEUTRAL, IMU_GYRO_R_NEUTRAL);
VECT3_ASSIGN(imu.accel_neutral, IMU_ACCEL_X_NEUTRAL, IMU_ACCEL_Y_NEUTRAL, IMU_ACCEL_Z_NEUTRAL);
#if defined IMU_MAG_X_NEUTRAL && defined IMU_MAG_Y_NEUTRAL && defined IMU_MAG_Z_NEUTRAL
VECT3_ASSIGN(imu.mag_neutral, IMU_MAG_X_NEUTRAL, IMU_MAG_Y_NEUTRAL, IMU_MAG_Z_NEUTRAL);
#else
#if USE_MAGNETOMETER
#pragma message "Info: Magnetomter neutrals are set to zero!"
#endif
INT_VECT3_ZERO(imu.mag_neutral);
#endif
/*
Compute quaternion and rotation matrix
for conversions between body and imu frame
*/
struct Int32Eulers body_to_imu_eulers =
{ ANGLE_BFP_OF_REAL(IMU_BODY_TO_IMU_PHI),
ANGLE_BFP_OF_REAL(IMU_BODY_TO_IMU_THETA),
ANGLE_BFP_OF_REAL(IMU_BODY_TO_IMU_PSI) };
INT32_QUAT_OF_EULERS(imu.body_to_imu_quat, body_to_imu_eulers);
INT32_QUAT_NORMALIZE(imu.body_to_imu_quat);
INT32_RMAT_OF_EULERS(imu.body_to_imu_rmat, body_to_imu_eulers);
imu_impl_init();
}
// reset to "hover" setpoint
static void reset_sp_quat(int32_t _psi, int32_t _theta, struct Int32Quat *initial)
{
int32_t pitch_rotation_angle;
struct Int32Quat pitch_axis_quat;
struct Int32Quat pitch_rotated_quat, pitch_rotated_quat2;
struct Int32Vect3 y_axis = { 0, 1, 0 };
struct Int32Eulers rotated_eulers;
// compose rotation about Y axis (pitch axis) from hover
pitch_rotation_angle = ANGLE_BFP_OF_REAL(-QUAT_SETPOINT_HOVER_PITCH);
INT32_QUAT_OF_AXIS_ANGLE(pitch_axis_quat, y_axis, pitch_rotation_angle);
INT32_QUAT_COMP_NORM_SHORTEST(pitch_rotated_quat, *initial, pitch_axis_quat);
INT32_EULERS_OF_QUAT(rotated_eulers, pitch_rotated_quat);
// reset euler angles
rotated_eulers.theta = _theta;
rotated_eulers.phi = _psi;
INT32_QUAT_OF_EULERS(pitch_rotated_quat, rotated_eulers);
// compose rotation about Y axis (pitch axis) to hover
pitch_rotation_angle = ANGLE_BFP_OF_REAL(QUAT_SETPOINT_HOVER_PITCH);
INT32_QUAT_OF_AXIS_ANGLE(pitch_axis_quat, y_axis, pitch_rotation_angle);
INT32_QUAT_COMP_NORM_SHORTEST(pitch_rotated_quat2, pitch_rotated_quat, pitch_axis_quat);
// store result into setpoint
QUAT_COPY(stab_att_sp_quat, pitch_rotated_quat2);
}
/* Compute ltp to imu rotation in quaternion and rotation matrice representation
from the euler angle representation */
__attribute__ ((always_inline)) static inline void compute_imu_quat_and_rmat_from_euler(void) {
/* Compute LTP to IMU quaternion */
INT32_QUAT_OF_EULERS(ahrs.ltp_to_imu_quat, ahrs.ltp_to_imu_euler);
/* Compute LTP to IMU rotation matrix */
INT32_RMAT_OF_EULERS(ahrs.ltp_to_imu_rmat, ahrs.ltp_to_imu_euler);
}
void imu_init(void) {
#ifdef IMU_POWER_GPIO
gpio_setup_output(IMU_POWER_GPIO);
IMU_POWER_GPIO_ON(IMU_POWER_GPIO);
#endif
/* initialises neutrals */
RATES_ASSIGN(imu.gyro_neutral, IMU_GYRO_P_NEUTRAL, IMU_GYRO_Q_NEUTRAL, IMU_GYRO_R_NEUTRAL);
VECT3_ASSIGN(imu.accel_neutral, IMU_ACCEL_X_NEUTRAL, IMU_ACCEL_Y_NEUTRAL, IMU_ACCEL_Z_NEUTRAL);
#if defined IMU_MAG_X_NEUTRAL && defined IMU_MAG_Y_NEUTRAL && defined IMU_MAG_Z_NEUTRAL
VECT3_ASSIGN(imu.mag_neutral, IMU_MAG_X_NEUTRAL, IMU_MAG_Y_NEUTRAL, IMU_MAG_Z_NEUTRAL);
#else
#if USE_MAGNETOMETER
INFO("Magnetometer neutrals are set to zero, you should calibrate!")
#endif
INT_VECT3_ZERO(imu.mag_neutral);
#endif
/*
Compute quaternion and rotation matrix
for conversions between body and imu frame
*/
struct Int32Eulers body_to_imu_eulers =
{ ANGLE_BFP_OF_REAL(IMU_BODY_TO_IMU_PHI),
ANGLE_BFP_OF_REAL(IMU_BODY_TO_IMU_THETA),
ANGLE_BFP_OF_REAL(IMU_BODY_TO_IMU_PSI) };
INT32_QUAT_OF_EULERS(imu.body_to_imu_quat, body_to_imu_eulers);
INT32_QUAT_NORMALIZE(imu.body_to_imu_quat);
INT32_RMAT_OF_EULERS(imu.body_to_imu_rmat, body_to_imu_eulers);
#if PERIODIC_TELEMETRY
register_periodic_telemetry(DefaultPeriodic, "IMU_ACCEL", send_accel);
register_periodic_telemetry(DefaultPeriodic, "IMU_GYRO", send_gyro);
#if USE_IMU_FLOAT
#else // !USE_IMU_FLOAT
register_periodic_telemetry(DefaultPeriodic, "IMU_ACCEL_RAW", send_accel_raw);
register_periodic_telemetry(DefaultPeriodic, "IMU_ACCEL_SCALED", send_accel_scaled);
register_periodic_telemetry(DefaultPeriodic, "IMU_ACCEL", send_accel);
register_periodic_telemetry(DefaultPeriodic, "IMU_GYRO_RAW", send_gyro_raw);
register_periodic_telemetry(DefaultPeriodic, "IMU_GYRO_SCALED", send_gyro_scaled);
register_periodic_telemetry(DefaultPeriodic, "IMU_GYRO", send_gyro);
register_periodic_telemetry(DefaultPeriodic, "IMU_MAG_RAW", send_mag_raw);
register_periodic_telemetry(DefaultPeriodic, "IMU_MAG_SCALED", send_mag_scaled);
register_periodic_telemetry(DefaultPeriodic, "IMU_MAG", send_mag);
#endif // !USE_IMU_FLOAT
#endif // DOWNLINK
imu_impl_init();
}
static void test_2(void) {
struct Int32Vect3 v1 = { 5000, 5000, 5000 };
DISPLAY_INT32_VECT3("v1", v1);
struct FloatEulers euler_f = { RadOfDeg(45.), RadOfDeg(0.), RadOfDeg(0.)};
DISPLAY_FLOAT_EULERS("euler_f", euler_f);
struct Int32Eulers euler_i;
EULERS_BFP_OF_REAL(euler_i, euler_f);
DISPLAY_INT32_EULERS("euler_i", euler_i);
struct Int32Quat quat_i;
INT32_QUAT_OF_EULERS(quat_i, euler_i);
DISPLAY_INT32_QUAT("quat_i", quat_i);
INT32_QUAT_NORMALIZE(quat_i);
DISPLAY_INT32_QUAT("quat_i_n", quat_i);
struct Int32Vect3 v2;
INT32_QUAT_VMULT(v2, quat_i, v1);
DISPLAY_INT32_VECT3("v2", v2);
struct Int32RMat rmat_i;
INT32_RMAT_OF_QUAT(rmat_i, quat_i);
DISPLAY_INT32_RMAT("rmat_i", rmat_i);
struct Int32Vect3 v3;
INT32_RMAT_VMULT(v3, rmat_i, v1);
DISPLAY_INT32_VECT3("v3", v3);
struct Int32RMat rmat_i2;
INT32_RMAT_OF_EULERS(rmat_i2, euler_i);
DISPLAY_INT32_RMAT("rmat_i2", rmat_i2);
struct Int32Vect3 v4;
INT32_RMAT_VMULT(v4, rmat_i2, v1);
DISPLAY_INT32_VECT3("v4", v4);
struct FloatQuat quat_f;
FLOAT_QUAT_OF_EULERS(quat_f, euler_f);
DISPLAY_FLOAT_QUAT("quat_f", quat_f);
struct FloatVect3 v5;
VECT3_COPY(v5, v1);
DISPLAY_FLOAT_VECT3("v5", v5);
struct FloatVect3 v6;
FLOAT_QUAT_VMULT(v6, quat_f, v5);
DISPLAY_FLOAT_VECT3("v6", v6);
}
static void test_1(void) {
struct FloatEulers euler_f = { RadOfDeg(45.), RadOfDeg(0.), RadOfDeg(0.)};
DISPLAY_FLOAT_EULERS("euler_f", euler_f);
struct Int32Eulers euler_i;
EULERS_BFP_OF_REAL(euler_i, euler_f);
DISPLAY_INT32_EULERS("euler_i", euler_i);
struct FloatQuat quat_f;
FLOAT_QUAT_OF_EULERS(quat_f, euler_f);
DISPLAY_FLOAT_QUAT("quat_f", quat_f);
struct Int32Quat quat_i;
INT32_QUAT_OF_EULERS(quat_i, euler_i);
DISPLAY_INT32_QUAT("quat_i", quat_i);
struct Int32RMat rmat_i;
INT32_RMAT_OF_QUAT(rmat_i, quat_i);
DISPLAY_INT32_RMAT("rmat_i", rmat_i);
}
static void test_4_int(void) {
printf("euler to quat to euler - int\n");
/* initial euler angles */
struct Int32Eulers _e;
EULERS_ASSIGN(_e, ANGLE_BFP_OF_REAL(RadOfDeg(-10.66)), ANGLE_BFP_OF_REAL(RadOfDeg(-0.7)), ANGLE_BFP_OF_REAL(RadOfDeg(0.)));
DISPLAY_INT32_EULERS_AS_FLOAT_DEG("euler orig ", _e);
/* transform to quaternion */
struct Int32Quat _q;
INT32_QUAT_OF_EULERS(_q, _e);
DISPLAY_INT32_QUAT_AS_EULERS_DEG("quat1 ", _q);
// INT32_QUAT_NORMALIZE(_q);
// DISPLAY_INT32_QUAT_2("_q_n", _q);
/* back to eulers */
struct Int32Eulers _e2;
INT32_EULERS_OF_QUAT(_e2, _q);
DISPLAY_INT32_EULERS_AS_FLOAT_DEG("back to euler ", _e2);
}
void stabilization_attitude_read_rc_absolute(bool_t in_flight) {
// FIXME: wtf???
#ifdef AIRPLANE_STICKS
pprz_t roll = radio_control.values[RADIO_ROLL];
pprz_t pitch = radio_control.values[RADIO_PITCH];
pprz_t yaw = radio_control.values[RADIO_YAW];
#else // QUAD STICKS
pprz_t roll = radio_control.values[RADIO_YAW];
pprz_t pitch = radio_control.values[RADIO_PITCH];
pprz_t yaw = -radio_control.values[RADIO_ROLL];
#endif
struct Int32Eulers sticks_eulers;
struct Int32Quat sticks_quat, prev_sp_quat;
// heading hold?
if (in_flight) {
// compose setpoint based on previous setpoint + pitch/roll sticks
reset_sp_quat(RATE_BFP_OF_REAL(yaw * YAW_COEF), RATE_BFP_OF_REAL(pitch * PITCH_COEF), &stab_att_sp_quat);
// get commanded yaw rate from sticks
sticks_eulers.phi = RATE_BFP_OF_REAL(APPLY_DEADBAND(roll, STABILIZATION_ATTITUDE_DEADBAND_A) * ROLL_COEF / RC_UPDATE_FREQ);
sticks_eulers.theta = 0;
sticks_eulers.psi = 0;
// convert yaw rate * dt into quaternion
INT32_QUAT_OF_EULERS(sticks_quat, sticks_eulers);
QUAT_COPY(prev_sp_quat, stab_att_sp_quat)
// update setpoint by rotating by incremental yaw command
INT32_QUAT_COMP_NORM_SHORTEST(stab_att_sp_quat, prev_sp_quat, sticks_quat);
} else { /* if not flying, use current body position + pitch/yaw from sticks to compose setpoint */
reset_sp_quat(RATE_BFP_OF_REAL(yaw * YAW_COEF), RATE_BFP_OF_REAL(pitch * PITCH_COEF), stateGetNedToBodyQuat_i());
}
// update euler setpoints for telemetry
INT32_EULERS_OF_QUAT(stab_att_sp_euler, stab_att_sp_quat);
}
static void test_3(void) {
/* Compute BODY to IMU eulers */
struct Int32Eulers b2i_e;
EULERS_ASSIGN(b2i_e, ANGLE_BFP_OF_REAL(RadOfDeg(10.66)), ANGLE_BFP_OF_REAL(RadOfDeg(-0.7)), ANGLE_BFP_OF_REAL(RadOfDeg(0.)));
DISPLAY_INT32_EULERS_AS_FLOAT_DEG("b2i_e", b2i_e);
/* Compute BODY to IMU quaternion */
struct Int32Quat b2i_q;
INT32_QUAT_OF_EULERS(b2i_q, b2i_e);
DISPLAY_INT32_QUAT_AS_EULERS_DEG("b2i_q", b2i_q);
// INT32_QUAT_NORMALIZE(b2i_q);
// DISPLAY_INT32_QUAT_AS_EULERS_DEG("b2i_q_n", b2i_q);
/* Compute BODY to IMU rotation matrix */
struct Int32RMat b2i_r;
INT32_RMAT_OF_EULERS(b2i_r, b2i_e);
// DISPLAY_INT32_RMAT("b2i_r", b2i_r);
DISPLAY_INT32_RMAT_AS_EULERS_DEG("b2i_r", b2i_r);
/* Compute LTP to IMU eulers */
struct Int32Eulers l2i_e;
EULERS_ASSIGN(l2i_e, ANGLE_BFP_OF_REAL(RadOfDeg(0.)), ANGLE_BFP_OF_REAL(RadOfDeg(20.)), ANGLE_BFP_OF_REAL(RadOfDeg(0.)));
DISPLAY_INT32_EULERS_AS_FLOAT_DEG("l2i_e", l2i_e);
/* Compute LTP to IMU quaternion */
struct Int32Quat l2i_q;
INT32_QUAT_OF_EULERS(l2i_q, l2i_e);
DISPLAY_INT32_QUAT_AS_EULERS_DEG("l2i_q", l2i_q);
/* Compute LTP to IMU rotation matrix */
struct Int32RMat l2i_r;
INT32_RMAT_OF_EULERS(l2i_r, l2i_e);
// DISPLAY_INT32_RMAT("l2i_r", l2i_r);
DISPLAY_INT32_RMAT_AS_EULERS_DEG("l2i_r", l2i_r);
/* again but from quaternion */
struct Int32RMat l2i_r2;
INT32_RMAT_OF_QUAT(l2i_r2, l2i_q);
// DISPLAY_INT32_RMAT("l2i_r2", l2i_r2);
DISPLAY_INT32_RMAT_AS_EULERS_DEG("l2i_r2", l2i_r2);
/* Compute LTP to BODY quaternion */
struct Int32Quat l2b_q;
INT32_QUAT_COMP_INV(l2b_q, b2i_q, l2i_q);
DISPLAY_INT32_QUAT_AS_EULERS_DEG("l2b_q", l2b_q);
/* Compute LTP to BODY rotation matrix */
struct Int32RMat l2b_r;
INT32_RMAT_COMP_INV(l2b_r, l2i_r, b2i_r);
// DISPLAY_INT32_RMAT("l2b_r", l2b_r);
DISPLAY_INT32_RMAT_AS_EULERS_DEG("l2b_r2", l2b_r);
/* again but from quaternion */
struct Int32RMat l2b_r2;
INT32_RMAT_OF_QUAT(l2b_r2, l2b_q);
// DISPLAY_INT32_RMAT("l2b_r2", l2b_r2);
DISPLAY_INT32_RMAT_AS_EULERS_DEG("l2b_r2", l2b_r2);
/* compute LTP to BODY eulers */
struct Int32Eulers l2b_e;
INT32_EULERS_OF_RMAT(l2b_e, l2b_r);
DISPLAY_INT32_EULERS_AS_FLOAT_DEG("l2b_e", l2b_e);
/* again but from quaternion */
struct Int32Eulers l2b_e2;
INT32_EULERS_OF_QUAT(l2b_e2, l2b_q);
DISPLAY_INT32_EULERS_AS_FLOAT_DEG("l2b_e2", l2b_e2);
}
void stabilization_attitude_set_from_eulers_i(struct Int32Eulers *sp_euler) {
// copy euler setpoint for debugging
memcpy(&stab_att_sp_euler, sp_euler, sizeof(struct Int32Eulers));
INT32_QUAT_OF_EULERS(stab_att_sp_quat, *sp_euler);
INT32_QUAT_WRAP_SHORTEST(stab_att_sp_quat);
}