static void send_inv_filter(struct transport_tx *trans, struct link_device *dev)
{
struct FloatEulers eulers;
struct FloatQuat quat = ins_mekf_wind_get_quat();
float_eulers_of_quat(&eulers, &quat);
//struct FloatRates rates = ins_mekf_wind_get_body_rates();
struct NedCoor_f pos = ins_mekf_wind_get_pos_ned();
struct NedCoor_f speed = ins_mekf_wind_get_speed_ned();
//struct NedCoor_f accel = ins_mekf_wind_get_accel_ned();
struct FloatVect3 ab = ins_mekf_wind_get_accel_bias();
struct FloatRates rb = ins_mekf_wind_get_rates_bias();
float airspeed = ins_mekf_wind_get_airspeed_norm();
pprz_msg_send_INV_FILTER(trans, dev,
AC_ID,
&quat.qi,
&eulers.phi,
&eulers.theta,
&eulers.psi,
&speed.x,
&speed.y,
&speed.z,
&pos.x,
&pos.y,
&pos.z,
&rb.p,
&rb.q,
&rb.r,
&ab.x,
&ab.y,
&ab.z,
&airspeed);
}
void ahrs_float_invariant_propagate(struct FloatRates* gyro, float dt)
{
// realign all the filter if needed
// a complete init cycle is required
if (ahrs_float_inv.reset) {
ahrs_float_inv.reset = false;
ahrs_float_inv.is_aligned = false;
init_invariant_state();
}
// fill command vector
struct FloatRates gyro_meas_body;
struct FloatRMat *body_to_imu_rmat = orientationGetRMat_f(&ahrs_float_inv.body_to_imu);
float_rmat_transp_ratemult(&gyro_meas_body, body_to_imu_rmat, gyro);
ahrs_float_inv.cmd.rates = gyro_meas_body;
// update correction gains
error_output(&ahrs_float_inv);
// propagate model
struct inv_state new_state;
runge_kutta_4_float((float *)&new_state,
(float *)&ahrs_float_inv.state, INV_STATE_DIM,
(float *)&ahrs_float_inv.cmd, INV_COMMAND_DIM,
invariant_model, dt);
ahrs_float_inv.state = new_state;
// normalize quaternion
float_quat_normalize(&ahrs_float_inv.state.quat);
//------------------------------------------------------------//
#if SEND_INVARIANT_FILTER
struct FloatEulers eulers;
float foo = 0.f;
float_eulers_of_quat(&eulers, &ahrs_float_inv.state.quat);
RunOnceEvery(3,
pprz_msg_send_INV_FILTER(&(DefaultChannel).trans_tx, &(DefaultDevice).device,
AC_ID,
&ahrs_float_inv.state.quat.qi,
&eulers.phi,
&eulers.theta,
&eulers.psi,
&foo,
&foo,
&foo,
&foo,
&foo,
&foo,
&ahrs_float_inv.state.bias.p,
&ahrs_float_inv.state.bias.q,
&ahrs_float_inv.state.bias.r,
&ahrs_float_inv.state.as,
&ahrs_float_inv.state.cs,
&foo,
&foo);
);
void ahrs_propagate(float dt)
{
struct FloatVect3 accel;
struct FloatRates body_rates;
// realign all the filter if needed
// a complete init cycle is required
if (ins_impl.reset) {
ins_impl.reset = FALSE;
ins.status = INS_UNINIT;
ahrs.status = AHRS_UNINIT;
init_invariant_state();
}
// fill command vector
struct Int32Rates gyro_meas_body;
struct Int32RMat *body_to_imu_rmat = orientationGetRMat_i(&imu.body_to_imu);
int32_rmat_transp_ratemult(&gyro_meas_body, body_to_imu_rmat, &imu.gyro);
RATES_FLOAT_OF_BFP(ins_impl.cmd.rates, gyro_meas_body);
struct Int32Vect3 accel_meas_body;
int32_rmat_transp_vmult(&accel_meas_body, body_to_imu_rmat, &imu.accel);
ACCELS_FLOAT_OF_BFP(ins_impl.cmd.accel, accel_meas_body);
// update correction gains
error_output(&ins_impl);
// propagate model
struct inv_state new_state;
runge_kutta_4_float((float *)&new_state,
(float *)&ins_impl.state, INV_STATE_DIM,
(float *)&ins_impl.cmd, INV_COMMAND_DIM,
invariant_model, dt);
ins_impl.state = new_state;
// normalize quaternion
FLOAT_QUAT_NORMALIZE(ins_impl.state.quat);
// set global state
stateSetNedToBodyQuat_f(&ins_impl.state.quat);
RATES_DIFF(body_rates, ins_impl.cmd.rates, ins_impl.state.bias);
stateSetBodyRates_f(&body_rates);
stateSetPositionNed_f(&ins_impl.state.pos);
stateSetSpeedNed_f(&ins_impl.state.speed);
// untilt accel and remove gravity
struct FloatQuat q_b2n;
float_quat_invert(&q_b2n, &ins_impl.state.quat);
float_quat_vmult(&accel, &q_b2n, &ins_impl.cmd.accel);
VECT3_SMUL(accel, accel, 1. / (ins_impl.state.as));
VECT3_ADD(accel, A);
stateSetAccelNed_f((struct NedCoor_f *)&accel);
//------------------------------------------------------------//
#if SEND_INVARIANT_FILTER
struct FloatEulers eulers;
FLOAT_EULERS_OF_QUAT(eulers, ins_impl.state.quat);
RunOnceEvery(3, {
pprz_msg_send_INV_FILTER(trans, dev, AC_ID,
&ins_impl.state.quat.qi,
&eulers.phi,
&eulers.theta,
&eulers.psi,
&ins_impl.state.speed.x,
&ins_impl.state.speed.y,
&ins_impl.state.speed.z,
&ins_impl.state.pos.x,
&ins_impl.state.pos.y,
&ins_impl.state.pos.z,
&ins_impl.state.bias.p,
&ins_impl.state.bias.q,
&ins_impl.state.bias.r,
&ins_impl.state.as,
&ins_impl.state.hb,
&ins_impl.meas.baro_alt,
&ins_impl.meas.pos_gps.z)
});
#endif
#if LOG_INVARIANT_FILTER
if (pprzLogFile.fs != NULL) {
if (!log_started) {
// log file header
sdLogWriteLog(&pprzLogFile,
"p q r ax ay az gx gy gz gvx gvy gvz mx my mz b qi qx qy qz bp bq br vx vy vz px py pz hb as\n");
log_started = TRUE;
} else {
sdLogWriteLog(&pprzLogFile,
"%.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f %.3f\n",
ins_impl.cmd.rates.p,
ins_impl.cmd.rates.q,
ins_impl.cmd.rates.r,
ins_impl.cmd.accel.x,
ins_impl.cmd.accel.y,
ins_impl.cmd.accel.z,
ins_impl.meas.pos_gps.x,
ins_impl.meas.pos_gps.y,
ins_impl.meas.pos_gps.z,
ins_impl.meas.speed_gps.x,
ins_impl.meas.speed_gps.y,
ins_impl.meas.speed_gps.z,
ins_impl.meas.mag.x,
ins_impl.meas.mag.y,
ins_impl.meas.mag.z,
ins_impl.meas.baro_alt,
ins_impl.state.quat.qi,
ins_impl.state.quat.qx,
ins_impl.state.quat.qy,
ins_impl.state.quat.qz,
ins_impl.state.bias.p,
ins_impl.state.bias.q,
ins_impl.state.bias.r,
ins_impl.state.speed.x,
ins_impl.state.speed.y,
ins_impl.state.speed.z,
ins_impl.state.pos.x,
ins_impl.state.pos.y,
ins_impl.state.pos.z,
ins_impl.state.hb,
ins_impl.state.as);
}
}
#endif
}
