void ins_propagate() {
/* untilt accels */
struct Int32Vect3 accel_meas_body;
INT32_RMAT_TRANSP_VMULT(accel_meas_body, imu.body_to_imu_rmat, imu.accel);
struct Int32Vect3 accel_meas_ltp;
INT32_RMAT_TRANSP_VMULT(accel_meas_ltp, (*stateGetNedToBodyRMat_i()), accel_meas_body);
#if USE_VFF
float z_accel_meas_float = ACCEL_FLOAT_OF_BFP(accel_meas_ltp.z);
if (baro.status == BS_RUNNING && ins_baro_initialised) {
vff_propagate(z_accel_meas_float);
ins_ltp_accel.z = ACCEL_BFP_OF_REAL(vff_zdotdot);
ins_ltp_speed.z = SPEED_BFP_OF_REAL(vff_zdot);
ins_ltp_pos.z = POS_BFP_OF_REAL(vff_z);
}
else { // feed accel from the sensors
// subtract -9.81m/s2 (acceleration measured due to gravity, but vehivle not accelerating in ltp)
ins_ltp_accel.z = accel_meas_ltp.z + ACCEL_BFP_OF_REAL(9.81);
}
#else
ins_ltp_accel.z = accel_meas_ltp.z + ACCEL_BFP_OF_REAL(9.81);
#endif /* USE_VFF */
#if USE_HFF
/* propagate horizontal filter */
b2_hff_propagate();
#else
ins_ltp_accel.x = accel_meas_ltp.x;
ins_ltp_accel.y = accel_meas_ltp.y;
#endif /* USE_HFF */
INS_NED_TO_STATE();
}
void ins_update_baro() {
#if USE_VFF
if (baro.status == BS_RUNNING) {
if (!ins_baro_initialised) {
ins_qfe = baro.absolute;
ins_baro_initialised = TRUE;
}
if (ins.vf_realign) {
ins.vf_realign = FALSE;
ins_qfe = baro.absolute;
#if USE_SONAR
ins_sonar_offset = sonar_meas;
#endif
vff_realign(0.);
ins_ltp_accel.z = ACCEL_BFP_OF_REAL(vff_zdotdot);
ins_ltp_speed.z = SPEED_BFP_OF_REAL(vff_zdot);
ins_ltp_pos.z = POS_BFP_OF_REAL(vff_z);
}
else { /* not realigning, so normal update with baro measurement */
ins_baro_alt = ((baro.absolute - ins_qfe) * INS_BARO_SENS_NUM)/INS_BARO_SENS_DEN;
float alt_float = POS_FLOAT_OF_BFP(ins_baro_alt);
vff_update(alt_float);
}
}
INS_NED_TO_STATE();
#endif
}
void ins_update_gps(void) {
#if USE_GPS
if (gps.fix == GPS_FIX_3D) {
if (!ins_ltp_initialised) {
ltp_def_from_ecef_i(&ins_ltp_def, &gps.ecef_pos);
ins_ltp_def.lla.alt = gps.lla_pos.alt;
ins_ltp_def.hmsl = gps.hmsl;
ins_ltp_initialised = TRUE;
stateSetLocalOrigin_i(&ins_ltp_def);
}
ned_of_ecef_point_i(&ins_gps_pos_cm_ned, &ins_ltp_def, &gps.ecef_pos);
ned_of_ecef_vect_i(&ins_gps_speed_cm_s_ned, &ins_ltp_def, &gps.ecef_vel);
#if USE_HFF
VECT2_ASSIGN(ins_gps_pos_m_ned, ins_gps_pos_cm_ned.x, ins_gps_pos_cm_ned.y);
VECT2_SDIV(ins_gps_pos_m_ned, ins_gps_pos_m_ned, 100.);
VECT2_ASSIGN(ins_gps_speed_m_s_ned, ins_gps_speed_cm_s_ned.x, ins_gps_speed_cm_s_ned.y);
VECT2_SDIV(ins_gps_speed_m_s_ned, ins_gps_speed_m_s_ned, 100.);
if (ins.hf_realign) {
ins.hf_realign = FALSE;
#ifdef SITL
struct FloatVect2 true_pos, true_speed;
VECT2_COPY(true_pos, fdm.ltpprz_pos);
VECT2_COPY(true_speed, fdm.ltpprz_ecef_vel);
b2_hff_realign(true_pos, true_speed);
#else
const struct FloatVect2 zero = {0.0, 0.0};
b2_hff_realign(ins_gps_pos_m_ned, zero);
#endif
}
b2_hff_update_gps();
#if !USE_VFF /* vff not used */
ins_ltp_pos.z = (ins_gps_pos_cm_ned.z * INT32_POS_OF_CM_NUM) / INT32_POS_OF_CM_DEN;
ins_ltp_speed.z = (ins_gps_speed_cm_s_ned.z * INT32_SPEED_OF_CM_S_NUM) INT32_SPEED_OF_CM_S_DEN;
#endif /* vff not used */
#endif /* hff used */
#if !USE_HFF /* hff not used */
#if !USE_VFF /* neither hf nor vf used */
INT32_VECT3_SCALE_3(ins_ltp_pos, ins_gps_pos_cm_ned, INT32_POS_OF_CM_NUM, INT32_POS_OF_CM_DEN);
INT32_VECT3_SCALE_3(ins_ltp_speed, ins_gps_speed_cm_s_ned, INT32_SPEED_OF_CM_S_NUM, INT32_SPEED_OF_CM_S_DEN);
#else /* only vff used */
INT32_VECT2_SCALE_2(ins_ltp_pos, ins_gps_pos_cm_ned, INT32_POS_OF_CM_NUM, INT32_POS_OF_CM_DEN);
INT32_VECT2_SCALE_2(ins_ltp_speed, ins_gps_speed_cm_s_ned, INT32_SPEED_OF_CM_S_NUM, INT32_SPEED_OF_CM_S_DEN);
#endif
#if USE_GPS_LAG_HACK
VECT2_COPY(d_pos, ins_ltp_speed);
INT32_VECT2_RSHIFT(d_pos, d_pos, 11);
VECT2_ADD(ins_ltp_pos, d_pos);
#endif
#endif /* hff not used */
INS_NED_TO_STATE();
}
#endif /* USE_GPS */
}
