Paparazzi UAS
v5.15_devel-230-gc96ce27
Paparazzi is a free software Unmanned Aircraft System.
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INS for rotorcrafts combining vertical and horizontal filters. More...
#include "subsystems/ins/ins_int.h"
#include "subsystems/abi.h"
#include "subsystems/imu.h"
#include "subsystems/gps.h"
#include "generated/airframe.h"
#include "subsystems/ins/vf_float.h"
#include "math/pprz_geodetic_int.h"
#include "math/pprz_isa.h"
#include "math/pprz_stat.h"
#include "subsystems/datalink/telemetry.h"
Go to the source code of this file.
Macros | |
#define | VFF_R_AGL 0.2 |
#define | INS_VFF_R_GPS 2.0 |
#define | INS_VFF_VZ_R_GPS 2.0 |
#define | INS_MAX_PROPAGATION_STEPS 200 |
maximum number of propagation steps without any updates in between More... | |
#define | USE_INS_NAV_INIT TRUE |
#define | INS_BARO_MAX_INIT_VAR 1.f |
default barometer to use in INS More... | |
#define | INS_INT_BARO_ID ABI_BROADCAST |
#define | INS_INT_IMU_ID ABI_BROADCAST |
ABI binding for IMU data. More... | |
#define | INS_INT_GPS_ID GPS_MULTI_ID |
#define | INS_INT_VEL_ID ABI_BROADCAST |
ABI binding for VELOCITY_ESTIMATE. More... | |
#define | INS_INT_POS_ID ABI_BROADCAST |
#define | INS_INT_AGL_ID ABI_BROADCAST |
ABI binding for AGL. More... | |
#define | press_hist_len 10 |
Functions | |
static void | baro_cb (uint8_t sender_id, uint32_t stamp, float pressure) |
static void | accel_cb (uint8_t sender_id, uint32_t stamp, struct Int32Vect3 *accel) |
static void | gps_cb (uint8_t sender_id, uint32_t stamp, struct GpsState *gps_s) |
static void | vel_est_cb (uint8_t sender_id, uint32_t stamp, float x, float y, float z, float noise_x, float noise_y, float noise_z) |
static void | pos_est_cb (uint8_t sender_id, uint32_t stamp, float x, float y, float z, float noise_x, float noise_y, float noise_z) |
static void | agl_cb (uint8_t sender_id, uint32_t stamp, float distance) |
agl_cb This callback handles all estimates of the height of the vehicle above the ground under it This is only used with the extended version of the vertical float filter More... | |
static void | send_ins (struct transport_tx *trans, struct link_device *dev) |
static void | send_ins_z (struct transport_tx *trans, struct link_device *dev) |
static void | send_ins_ref (struct transport_tx *trans, struct link_device *dev) |
static void | ins_ned_to_state (void) |
copy position and speed to state interface More... | |
static void | ins_update_from_vff (void) |
update ins state from vertical filter More... | |
void | ins_int_init (void) |
void | ins_reset_local_origin (void) |
INS local origin reset. More... | |
void | ins_reset_altitude_ref (void) |
INS altitude reference reset. More... | |
void | ins_int_propagate (struct Int32Vect3 *accel, float dt) |
void | ins_int_update_gps (struct GpsState *gps_s) |
Variables | |
abi_event | baro_ev |
static abi_event | accel_ev |
static abi_event | gps_ev |
static abi_event | vel_est_ev |
static abi_event | pos_est_ev |
static abi_event | agl_ev |
The agl ABI event. More... | |
struct InsInt | ins_int |
global INS state More... | |
INS for rotorcrafts combining vertical and horizontal filters.
Definition in file ins_int.c.
#define INS_BARO_MAX_INIT_VAR 1.f |
#define INS_INT_AGL_ID ABI_BROADCAST |
ABI binding for AGL.
Usually this is comes from sonar or gps.
Definition at line 161 of file ins_int.c.
Referenced by ins_int_init().
#define INS_INT_BARO_ID ABI_BROADCAST |
Definition at line 115 of file ins_int.c.
Referenced by ins_int_init().
#define INS_INT_GPS_ID GPS_MULTI_ID |
Definition at line 132 of file ins_int.c.
Referenced by ins_int_init().
#define INS_INT_IMU_ID ABI_BROADCAST |
ABI binding for IMU data.
Used accel ABI messages.
Definition at line 126 of file ins_int.c.
Referenced by ins_int_init().
#define INS_INT_POS_ID ABI_BROADCAST |
Definition at line 149 of file ins_int.c.
Referenced by ins_int_init().
#define INS_INT_VEL_ID ABI_BROADCAST |
ABI binding for VELOCITY_ESTIMATE.
Usually this is coming from opticflow.
Definition at line 141 of file ins_int.c.
Referenced by ins_int_init().
#define INS_MAX_PROPAGATION_STEPS 200 |
maximum number of propagation steps without any updates in between
Definition at line 101 of file ins_int.c.
Referenced by ins_int_init(), and ins_int_propagate().
#define INS_VFF_R_GPS 2.0 |
Definition at line 91 of file ins_int.c.
Referenced by ins_int_update_gps().
#define INS_VFF_VZ_R_GPS 2.0 |
Definition at line 95 of file ins_int.c.
Referenced by ins_int_update_gps().
#define press_hist_len 10 |
Referenced by baro_cb().
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Definition at line 549 of file ins_int.c.
References ins_int_propagate(), and PRINT_CONFIG_MSG().
Referenced by ins_int_init().
agl_cb This callback handles all estimates of the height of the vehicle above the ground under it This is only used with the extended version of the vertical float filter
Definition at line 510 of file ins_int.c.
Referenced by ins_int_init().
Definition at line 337 of file ins_int.c.
References InsInt::baro_initialized, InsInt::baro_z, idx, INS_BARO_MAX_INIT_VAR, ins_int, ins_update_from_vff(), InsInt::ltp_initialized, pprz_isa_height_of_pressure(), press_hist_len, InsInt::propagation_cnt, InsInt::qfe, stateGetPositionEnu_f(), variance_f(), InsInt::vf_reset, vff_realign(), vff_update(), vff_update_baro(), EnuCoor_f::x, and EnuCoor_f::y.
Referenced by ins_int_init().
Definition at line 563 of file ins_int.c.
References ins_int_update_gps().
Referenced by ins_int_init().
void ins_int_init | ( | void | ) |
Definition at line 203 of file ins_int.c.
References accel_cb(), agl_cb(), baro_cb(), InsInt::baro_initialized, DefaultPeriodic, gps_cb(), InsInt::hf_realign, hff_init(), ins_init_origin_i_from_flightplan(), ins_int, INS_INT_AGL_ID, INS_INT_BARO_ID, INS_INT_GPS_ID, INS_INT_IMU_ID, INS_INT_POS_ID, INS_INT_VEL_ID, INS_MAX_PROPAGATION_STEPS, INT32_VECT3_ZERO, InsInt::ltp_accel, InsInt::ltp_def, InsInt::ltp_initialized, InsInt::ltp_pos, InsInt::ltp_speed, pos_est_cb(), InsInt::propagation_cnt, register_periodic_telemetry(), send_ins(), send_ins_ref(), send_ins_z(), vel_est_cb(), InsInt::vf_reset, and vff_init_zero().
void ins_int_propagate | ( | struct Int32Vect3 * | accel, |
float | dt | ||
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Definition at line 292 of file ins_int.c.
References ACCEL_BFP_OF_REAL, ACCEL_FLOAT_OF_BFP, Imu::body_to_imu, hff_propagate(), imu, ins_int, INS_MAX_PROPAGATION_STEPS, ins_ned_to_state(), ins_update_from_vff(), int32_rmat_transp_vmult(), InsInt::ltp_accel, orientationGetRMat_i(), InsInt::propagation_cnt, stateGetNedToBodyRMat_i(), stateSetAccelBody_i(), vff_propagate(), NedCoor_i::x, Int32Vect3::x, NedCoor_i::y, Int32Vect3::y, NedCoor_i::z, and Int32Vect3::z.
Referenced by accel_cb().
void ins_int_update_gps | ( | struct GpsState * | gps_s | ) |
Definition at line 396 of file ins_int.c.
References GpsState::ecef_pos, GpsState::ecef_vel, GpsState::fix, GPS_FIX_3D, InsInt::hf_realign, hff_realign(), hff_update_gps(), ins_int, ins_ned_to_state(), ins_reset_local_origin(), INS_VFF_R_GPS, INS_VFF_VZ_R_GPS, INT32_POS_OF_CM_DEN, INT32_POS_OF_CM_NUM, int32_quat_vmult(), INT32_SPEED_OF_CM_S_DEN, INT32_SPEED_OF_CM_S_NUM, INT32_VECT2_SCALE_2, InsInt::ltp_def, InsInt::ltp_initialized, InsInt::ltp_pos, InsInt::ltp_speed, ned_of_ecef_point_i(), ned_of_ecef_vect_i(), InsInt::propagation_cnt, QUAT_INVERT, stateGetNedToBodyQuat_i(), VECT2_ASSIGN, VECT2_SDIV, VECT3_SUB, vff_update_vz_conf(), vff_update_z_conf(), NedCoor_i::x, Int32Vect3::x, NedCoor_i::y, and NedCoor_i::z.
Referenced by gps_cb().
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copy position and speed to state interface
Definition at line 514 of file ins_int.c.
References ins_int, InsInt::ltp_accel, InsInt::ltp_pos, InsInt::ltp_speed, nps_bypass_ins, sim_overwrite_ins(), stateSetAccelNed_i(), stateSetPositionNed_i(), and stateSetSpeedNed_i().
Referenced by ins_int_propagate(), ins_int_update_gps(), pos_est_cb(), and vel_est_cb().
void ins_reset_altitude_ref | ( | void | ) |
INS altitude reference reset.
Reset only vertical reference to the current altitude. Does nothing if not implemented by specific INS algorithm.
Definition at line 275 of file ins_int.c.
References LlaCoor_i::alt, gps, GpsFixValid, GpsState::hmsl, LtpDef_i::hmsl, ins_int, LlaCoor_i::lat, LtpDef_i::lla, GpsState::lla_pos, LlaCoor_i::lon, InsInt::ltp_def, ltp_def_from_lla_i(), State::ned_origin_i, state, stateSetLocalOrigin_i(), and InsInt::vf_reset.
void ins_reset_local_origin | ( | void | ) |
INS local origin reset.
Reset horizontal and vertical reference to the current position. Does nothing if not implemented by specific INS algorithm.
INS local origin reset.
Definition at line 253 of file ins_int.c.
References LlaCoor_i::alt, GpsState::ecef_pos, gps, GpsFixValid, InsInt::hf_realign, GpsState::hmsl, LtpDef_i::hmsl, ins_int, LtpDef_i::lla, GpsState::lla_pos, InsInt::ltp_def, ltp_def_from_ecef_i(), InsInt::ltp_initialized, stateSetLocalOrigin_i(), and InsInt::vf_reset.
Referenced by ins_int_update_gps().
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update ins state from vertical filter
Definition at line 528 of file ins_int.c.
References ACCEL_BFP_OF_REAL, ins_int, InsInt::ltp_accel, InsInt::ltp_pos, InsInt::ltp_speed, POS_BFP_OF_REAL, SPEED_BFP_OF_REAL, vff, VffExtended::z, NedCoor_i::z, VffExtended::zdot, and VffExtended::zdotdot.
Referenced by baro_cb(), and ins_int_propagate().
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Definition at line 635 of file ins_int.c.
References hff_update_pos(), ins_int, ins_ned_to_state(), InsInt::ltp_pos, POS_BFP_OF_REAL, InsInt::propagation_cnt, vff_update_z_conf(), FloatVect2::x, NedCoor_i::x, and NedCoor_i::y.
Referenced by ins_int_init().
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Definition at line 171 of file ins_int.c.
References ins_int, InsInt::ltp_accel, InsInt::ltp_pos, InsInt::ltp_speed, NedCoor_i::x, NedCoor_i::y, and NedCoor_i::z.
Referenced by ins_int_init().
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Definition at line 185 of file ins_int.c.
References LlaCoor_i::alt, LtpDef_i::ecef, LtpDef_i::hmsl, ins_int, LlaCoor_i::lat, LtpDef_i::lla, LlaCoor_i::lon, InsInt::ltp_def, InsInt::ltp_initialized, InsInt::qfe, EcefCoor_i::x, EcefCoor_i::y, and EcefCoor_i::z.
Referenced by ins_int_init().
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Definition at line 179 of file ins_int.c.
References InsInt::baro_z, ins_int, InsInt::ltp_accel, InsInt::ltp_pos, InsInt::ltp_speed, and NedCoor_i::z.
Referenced by ins_int_init().
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Definition at line 573 of file ins_int.c.
References float_quat_vmult(), hff_update_vel(), ins_int, ins_ned_to_state(), InsInt::ltp_pos, InsInt::ltp_speed, POS_BFP_OF_REAL, InsInt::propagation_cnt, QUAT_INVERT, SPEED_BFP_OF_REAL, stateGetNedToBodyQuat_f(), vff_update_vz_conf(), FloatVect3::x, NedCoor_i::x, FloatVect3::y, NedCoor_i::y, and FloatVect3::z.
Referenced by ins_int_init().
struct InsInt ins_int |
global INS state
Definition at line 166 of file ins_int.c.
Referenced by baro_cb(), ins_int_init(), ins_int_propagate(), ins_int_update_gps(), ins_ned_to_state(), ins_reset_altitude_ref(), ins_reset_local_origin(), ins_update_from_vff(), pos_est_cb(), send_ins(), send_ins_ref(), send_ins_z(), and vel_est_cb().