void nps_autopilot_run_step(double time)
{
nps_electrical_run_step(time);
#if RADIO_CONTROL && !RADIO_CONTROL_TYPE_DATALINK
if (nps_radio_control_available(time)) {
radio_control_feed();
main_event();
}
#endif
if (nps_sensors_gyro_available()) {
imu_feed_gyro_accel();
main_event();
}
if (nps_sensors_mag_available()) {
imu_feed_mag();
main_event();
}
if (nps_sensors_baro_available()) {
float pressure = (float) sensors.baro.value;
AbiSendMsgBARO_ABS(BARO_SIM_SENDER_ID, pressure);
main_event();
}
#if USE_SONAR
if (nps_sensors_sonar_available()) {
float dist = (float) sensors.sonar.value;
AbiSendMsgAGL(AGL_SONAR_NPS_ID, dist);
uint16_t foo = 0;
DOWNLINK_SEND_SONAR(DefaultChannel, DefaultDevice, &foo, &dist);
main_event();
}
#endif
if (nps_sensors_gps_available()) {
gps_feed_value();
main_event();
}
if (nps_bypass_ahrs) {
sim_overwrite_ahrs();
}
if (nps_bypass_ins) {
sim_overwrite_ins();
}
handle_periodic_tasks();
/* scale final motor commands to 0-1 for feeding the fdm */
for (uint8_t i = 0; i < NPS_COMMANDS_NB; i++) {
autopilot.commands[i] = (double)motor_mixing.commands[i] / MAX_PPRZ;
}
}
/** copy position and speed to state interface */
static void ins_ned_to_state(void)
{
stateSetPositionNed_i(&ins_module.ltp_pos);
stateSetSpeedNed_i(&ins_module.ltp_speed);
stateSetAccelNed_i(&ins_module.ltp_accel);
#if defined SITL && USE_NPS
if (nps_bypass_ins) {
sim_overwrite_ins();
}
#endif
}
void ins_reset_altitude_ref(void)
{
#if USE_GPS
struct LlaCoor_i lla = {
.lat = state.ned_origin_i.lla.lat,
.lon = state.ned_origin_i.lla.lon,
.alt = gps.lla_pos.alt
};
ltp_def_from_lla_i(&ins_impl.ltp_def, &lla);
ins_impl.ltp_def.hmsl = gps.hmsl;
stateSetLocalOrigin_i(&ins_impl.ltp_def);
#endif
ins_impl.vf_reset = TRUE;
}
void ins_propagate(float dt)
{
/* untilt accels */
struct Int32Vect3 accel_meas_body;
struct Int32RMat *body_to_imu_rmat = orientationGetRMat_i(&imu.body_to_imu);
int32_rmat_transp_vmult(&accel_meas_body, body_to_imu_rmat, &imu.accel);
struct Int32Vect3 accel_meas_ltp;
int32_rmat_transp_vmult(&accel_meas_ltp, stateGetNedToBodyRMat_i(), &accel_meas_body);
float z_accel_meas_float = ACCEL_FLOAT_OF_BFP(accel_meas_ltp.z);
if (ins_impl.baro_initialized) {
vff_propagate(z_accel_meas_float, dt);
ins_update_from_vff();
} else { // feed accel from the sensors
// subtract -9.81m/s2 (acceleration measured due to gravity,
// but vehicle not accelerating in ltp)
ins_impl.ltp_accel.z = accel_meas_ltp.z + ACCEL_BFP_OF_REAL(9.81);
}
#if USE_HFF
/* propagate horizontal filter */
b2_hff_propagate();
/* convert and copy result to ins_impl */
ins_update_from_hff();
#else
ins_impl.ltp_accel.x = accel_meas_ltp.x;
ins_impl.ltp_accel.y = accel_meas_ltp.y;
#endif /* USE_HFF */
ins_ned_to_state();
}
static void baro_cb(uint8_t __attribute__((unused)) sender_id, const float *pressure)
{
if (!ins_impl.baro_initialized && *pressure > 1e-7) {
// wait for a first positive value
ins_impl.qfe = *pressure;
ins_impl.baro_initialized = TRUE;
}
if (ins_impl.baro_initialized) {
if (ins_impl.vf_reset) {
ins_impl.vf_reset = FALSE;
ins_impl.qfe = *pressure;
vff_realign(0.);
ins_update_from_vff();
} else {
ins_impl.baro_z = -pprz_isa_height_of_pressure(*pressure, ins_impl.qfe);
#if USE_VFF_EXTENDED
vff_update_baro(ins_impl.baro_z);
#else
vff_update(ins_impl.baro_z);
#endif
}
ins_ned_to_state();
}
}
#if USE_GPS
void ins_update_gps(void)
{
if (gps.fix == GPS_FIX_3D) {
if (!ins_impl.ltp_initialized) {
ltp_def_from_ecef_i(&ins_impl.ltp_def, &gps.ecef_pos);
ins_impl.ltp_def.lla.alt = gps.lla_pos.alt;
ins_impl.ltp_def.hmsl = gps.hmsl;
ins_impl.ltp_initialized = TRUE;
stateSetLocalOrigin_i(&ins_impl.ltp_def);
}
struct NedCoor_i gps_pos_cm_ned;
ned_of_ecef_point_i(&gps_pos_cm_ned, &ins_impl.ltp_def, &gps.ecef_pos);
/// @todo maybe use gps.ned_vel directly??
struct NedCoor_i gps_speed_cm_s_ned;
ned_of_ecef_vect_i(&gps_speed_cm_s_ned, &ins_impl.ltp_def, &gps.ecef_vel);
#if INS_USE_GPS_ALT
vff_update_z_conf((float)gps_pos_cm_ned.z / 100.0, INS_VFF_R_GPS);
#endif
#if USE_HFF
/* horizontal gps transformed to NED in meters as float */
struct FloatVect2 gps_pos_m_ned;
VECT2_ASSIGN(gps_pos_m_ned, gps_pos_cm_ned.x, gps_pos_cm_ned.y);
VECT2_SDIV(gps_pos_m_ned, gps_pos_m_ned, 100.0f);
struct FloatVect2 gps_speed_m_s_ned;
VECT2_ASSIGN(gps_speed_m_s_ned, gps_speed_cm_s_ned.x, gps_speed_cm_s_ned.y);
VECT2_SDIV(gps_speed_m_s_ned, gps_speed_m_s_ned, 100.);
if (ins_impl.hf_realign) {
ins_impl.hf_realign = FALSE;
const struct FloatVect2 zero = {0.0f, 0.0f};
b2_hff_realign(gps_pos_m_ned, zero);
}
// run horizontal filter
b2_hff_update_gps(&gps_pos_m_ned, &gps_speed_m_s_ned);
// convert and copy result to ins_impl
ins_update_from_hff();
#else /* hff not used */
/* simply copy horizontal pos/speed from gps */
INT32_VECT2_SCALE_2(ins_impl.ltp_pos, gps_pos_cm_ned,
INT32_POS_OF_CM_NUM, INT32_POS_OF_CM_DEN);
INT32_VECT2_SCALE_2(ins_impl.ltp_speed, gps_speed_cm_s_ned,
INT32_SPEED_OF_CM_S_NUM, INT32_SPEED_OF_CM_S_DEN);
#endif /* USE_HFF */
ins_ned_to_state();
}
}
#endif /* USE_GPS */
#if USE_SONAR
static void sonar_cb(uint8_t __attribute__((unused)) sender_id, const float *distance)
{
static float last_offset = 0.;
/* update filter assuming a flat ground */
if (*distance < INS_SONAR_MAX_RANGE && *distance > INS_SONAR_MIN_RANGE
#ifdef INS_SONAR_THROTTLE_THRESHOLD
&& stabilization_cmd[COMMAND_THRUST] < INS_SONAR_THROTTLE_THRESHOLD
#endif
#ifdef INS_SONAR_BARO_THRESHOLD
&& ins_impl.baro_z > -INS_SONAR_BARO_THRESHOLD /* z down */
#endif
&& ins_impl.update_on_agl
&& ins_impl.baro_initialized) {
vff_update_z_conf(-(*distance), VFF_R_SONAR_0 + VFF_R_SONAR_OF_M * fabsf(*distance));
last_offset = vff.offset;
} else {
/* update offset with last value to avoid divergence */
vff_update_offset(last_offset);
}
}
#endif // USE_SONAR
/** initialize the local origin (ltp_def) from flight plan position */
static void ins_init_origin_from_flightplan(void)
{
struct LlaCoor_i llh_nav0; /* Height above the ellipsoid */
llh_nav0.lat = NAV_LAT0;
llh_nav0.lon = NAV_LON0;
/* NAV_ALT0 = ground alt above msl, NAV_MSL0 = geoid-height (msl) over ellipsoid */
llh_nav0.alt = NAV_ALT0 + NAV_MSL0;
struct EcefCoor_i ecef_nav0;
ecef_of_lla_i(&ecef_nav0, &llh_nav0);
ltp_def_from_ecef_i(&ins_impl.ltp_def, &ecef_nav0);
ins_impl.ltp_def.hmsl = NAV_ALT0;
stateSetLocalOrigin_i(&ins_impl.ltp_def);
}
/** copy position and speed to state interface */
static void ins_ned_to_state(void)
{
stateSetPositionNed_i(&ins_impl.ltp_pos);
stateSetSpeedNed_i(&ins_impl.ltp_speed);
stateSetAccelNed_i(&ins_impl.ltp_accel);
#if defined SITL && USE_NPS
if (nps_bypass_ins) {
sim_overwrite_ins();
}
#endif
}
void ins_reset_altitude_ref(void)
{
#if USE_GPS
struct LlaCoor_i lla = {
.lat = state.ned_origin_i.lla.lat,
.lon = state.ned_origin_i.lla.lon,
.alt = gps.lla_pos.alt
};
ltp_def_from_lla_i(&ins_int.ltp_def, &lla);
ins_int.ltp_def.hmsl = gps.hmsl;
stateSetLocalOrigin_i(&ins_int.ltp_def);
#endif
ins_int.vf_reset = TRUE;
}
void ins_int_propagate(struct Int32Vect3 *accel, float dt)
{
/* untilt accels */
struct Int32Vect3 accel_meas_body;
struct Int32RMat *body_to_imu_rmat = orientationGetRMat_i(&imu.body_to_imu);
int32_rmat_transp_vmult(&accel_meas_body, body_to_imu_rmat, accel);
struct Int32Vect3 accel_meas_ltp;
int32_rmat_transp_vmult(&accel_meas_ltp, stateGetNedToBodyRMat_i(), &accel_meas_body);
float z_accel_meas_float = ACCEL_FLOAT_OF_BFP(accel_meas_ltp.z);
/* Propagate only if we got any measurement during the last INS_MAX_PROPAGATION_STEPS.
* Otherwise halt the propagation to not diverge and only set the acceleration.
* This should only be relevant in the startup phase when the baro is not yet initialized
* and there is no gps fix yet...
*/
if (ins_int.propagation_cnt < INS_MAX_PROPAGATION_STEPS) {
vff_propagate(z_accel_meas_float, dt);
ins_update_from_vff();
} else {
// feed accel from the sensors
// subtract -9.81m/s2 (acceleration measured due to gravity,
// but vehicle not accelerating in ltp)
ins_int.ltp_accel.z = accel_meas_ltp.z + ACCEL_BFP_OF_REAL(9.81);
}
#if USE_HFF
/* propagate horizontal filter */
b2_hff_propagate();
/* convert and copy result to ins_int */
ins_update_from_hff();
#else
ins_int.ltp_accel.x = accel_meas_ltp.x;
ins_int.ltp_accel.y = accel_meas_ltp.y;
#endif /* USE_HFF */
ins_ned_to_state();
/* increment the propagation counter, while making sure it doesn't overflow */
if (ins_int.propagation_cnt < 100 * INS_MAX_PROPAGATION_STEPS) {
ins_int.propagation_cnt++;
}
}
static void baro_cb(uint8_t __attribute__((unused)) sender_id, float pressure)
{
if (!ins_int.baro_initialized && pressure > 1e-7) {
// wait for a first positive value
ins_int.qfe = pressure;
ins_int.baro_initialized = TRUE;
}
if (ins_int.baro_initialized) {
if (ins_int.vf_reset) {
ins_int.vf_reset = FALSE;
ins_int.qfe = pressure;
vff_realign(0.);
ins_update_from_vff();
} else {
ins_int.baro_z = -pprz_isa_height_of_pressure(pressure, ins_int.qfe);
#if USE_VFF_EXTENDED
vff_update_baro(ins_int.baro_z);
#else
vff_update(ins_int.baro_z);
#endif
}
ins_ned_to_state();
/* reset the counter to indicate we just had a measurement update */
ins_int.propagation_cnt = 0;
}
}
#if USE_GPS
void ins_int_update_gps(struct GpsState *gps_s)
{
if (gps_s->fix < GPS_FIX_3D) {
return;
}
if (!ins_int.ltp_initialized) {
ins_reset_local_origin();
}
struct NedCoor_i gps_pos_cm_ned;
ned_of_ecef_point_i(&gps_pos_cm_ned, &ins_int.ltp_def, &gps_s->ecef_pos);
/* calculate body frame position taking BODY_TO_GPS translation (in cm) into account */
#ifdef INS_BODY_TO_GPS_X
/* body2gps translation in body frame */
struct Int32Vect3 b2g_b = {
.x = INS_BODY_TO_GPS_X,
.y = INS_BODY_TO_GPS_Y,
.z = INS_BODY_TO_GPS_Z
};
/* rotate offset given in body frame to navigation/ltp frame using current attitude */
struct Int32Quat q_b2n = *stateGetNedToBodyQuat_i();
QUAT_INVERT(q_b2n, q_b2n);
struct Int32Vect3 b2g_n;
int32_quat_vmult(&b2g_n, &q_b2n, &b2g_b);
/* subtract body2gps translation in ltp from gps position */
VECT3_SUB(gps_pos_cm_ned, b2g_n);
#endif
/// @todo maybe use gps_s->ned_vel directly??
struct NedCoor_i gps_speed_cm_s_ned;
ned_of_ecef_vect_i(&gps_speed_cm_s_ned, &ins_int.ltp_def, &gps_s->ecef_vel);
#if INS_USE_GPS_ALT
vff_update_z_conf(((float)gps_pos_cm_ned.z) / 100.0, INS_VFF_R_GPS);
#endif
#if INS_USE_GPS_ALT_SPEED
vff_update_vz_conf(((float)gps_speed_cm_s_ned.z) / 100.0, INS_VFF_VZ_R_GPS);
#endif
#if USE_HFF
/* horizontal gps transformed to NED in meters as float */
struct FloatVect2 gps_pos_m_ned;
VECT2_ASSIGN(gps_pos_m_ned, gps_pos_cm_ned.x, gps_pos_cm_ned.y);
VECT2_SDIV(gps_pos_m_ned, gps_pos_m_ned, 100.0f);
struct FloatVect2 gps_speed_m_s_ned;
VECT2_ASSIGN(gps_speed_m_s_ned, gps_speed_cm_s_ned.x, gps_speed_cm_s_ned.y);
VECT2_SDIV(gps_speed_m_s_ned, gps_speed_m_s_ned, 100.);
if (ins_int.hf_realign) {
ins_int.hf_realign = FALSE;
const struct FloatVect2 zero = {0.0f, 0.0f};
b2_hff_realign(gps_pos_m_ned, zero);
}
// run horizontal filter
b2_hff_update_gps(&gps_pos_m_ned, &gps_speed_m_s_ned);
// convert and copy result to ins_int
ins_update_from_hff();
#else /* hff not used */
/* simply copy horizontal pos/speed from gps */
INT32_VECT2_SCALE_2(ins_int.ltp_pos, gps_pos_cm_ned,
INT32_POS_OF_CM_NUM, INT32_POS_OF_CM_DEN);
INT32_VECT2_SCALE_2(ins_int.ltp_speed, gps_speed_cm_s_ned,
INT32_SPEED_OF_CM_S_NUM, INT32_SPEED_OF_CM_S_DEN);
#endif /* USE_HFF */
ins_ned_to_state();
/* reset the counter to indicate we just had a measurement update */
ins_int.propagation_cnt = 0;
}
#else
void ins_int_update_gps(struct GpsState *gps_s __attribute__((unused))) {}
#endif /* USE_GPS */
#if USE_SONAR
static void sonar_cb(uint8_t __attribute__((unused)) sender_id, float distance)
{
static float last_offset = 0.;
/* update filter assuming a flat ground */
if (distance < INS_SONAR_MAX_RANGE && distance > INS_SONAR_MIN_RANGE
#ifdef INS_SONAR_THROTTLE_THRESHOLD
&& stabilization_cmd[COMMAND_THRUST] < INS_SONAR_THROTTLE_THRESHOLD
#endif
#ifdef INS_SONAR_BARO_THRESHOLD
&& ins_int.baro_z > -INS_SONAR_BARO_THRESHOLD /* z down */
#endif
&& ins_int.update_on_agl
&& ins_int.baro_initialized) {
vff_update_z_conf(-(distance), VFF_R_SONAR_0 + VFF_R_SONAR_OF_M * fabsf(distance));
last_offset = vff.offset;
} else {
/* update offset with last value to avoid divergence */
vff_update_offset(last_offset);
}
/* reset the counter to indicate we just had a measurement update */
ins_int.propagation_cnt = 0;
}
#endif // USE_SONAR
/** initialize the local origin (ltp_def) from flight plan position */
static void ins_init_origin_from_flightplan(void)
{
struct LlaCoor_i llh_nav0; /* Height above the ellipsoid */
llh_nav0.lat = NAV_LAT0;
llh_nav0.lon = NAV_LON0;
/* NAV_ALT0 = ground alt above msl, NAV_MSL0 = geoid-height (msl) over ellipsoid */
llh_nav0.alt = NAV_ALT0 + NAV_MSL0;
struct EcefCoor_i ecef_nav0;
ecef_of_lla_i(&ecef_nav0, &llh_nav0);
ltp_def_from_ecef_i(&ins_int.ltp_def, &ecef_nav0);
ins_int.ltp_def.hmsl = NAV_ALT0;
stateSetLocalOrigin_i(&ins_int.ltp_def);
}
/** copy position and speed to state interface */
static void ins_ned_to_state(void)
{
stateSetPositionNed_i(&ins_int.ltp_pos);
stateSetSpeedNed_i(&ins_int.ltp_speed);
stateSetAccelNed_i(&ins_int.ltp_accel);
#if defined SITL && USE_NPS
if (nps_bypass_ins) {
sim_overwrite_ins();
}
#endif
}
