ins_int.h File Reference

INS for rotorcrafts combining vertical and horizontal filters. More...

#include "modules/ins/ins.h"
#include "modules/gps/gps.h"
#include "std.h"
#include "math/pprz_geodetic_int.h"
#include "math/pprz_algebra_float.h"

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Data Structures
struct	InsInt
	Ins implementation state (fixed point) More...

Functions
void	ins_int_init (void)
void	ins_int_propagate (struct Int32Vect3 *accel, float dt)
void	ins_int_update_gps (struct GpsState *gps_s)

Variables
struct InsInt	ins_int
	global INS state More...

Detailed Description

INS for rotorcrafts combining vertical and horizontal filters.

Definition in file ins_int.h.

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Data Structure Documentation

InsInt

struct InsInt

Ins implementation state (fixed point)

Definition at line 39 of file ins_int.h.

Collaboration diagram for InsInt:

Data Fields
bool	baro_initialized
float	baro_z	z-position calculated from baro in meters (z-down)
bool	hf_realign	request to realign horizontal filter. Sets to current position (local origin unchanged).
struct NedCoor_i	ltp_accel
struct LtpDef_i	ltp_def
bool	ltp_initialized
struct NedCoor_i	ltp_pos
struct NedCoor_i	ltp_speed
uint32_t	propagation_cnt	number of propagation steps since the last measurement update
float	qfe
bool	vf_reset	request to reset vertical filter. Sets the z-position to zero and resets the the z-reference to current altitude.

Function Documentation

ins_int_init()

void ins_int_init

(

void

)

Definition at line 207 of file ins_int.c.

References ABI_BROADCAST, accel_cb(), accel_ev, agl_cb(), agl_ev, baro_cb(), baro_ev, InsInt::baro_initialized, DefaultPeriodic, gps_cb(), gps_ev, 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(), pos_est_ev, InsInt::propagation_cnt, register_periodic_telemetry(), reset_cb(), reset_ev, send_ins(), send_ins_ref(), send_ins_z(), vel_est_cb(), vel_est_ev, InsInt::vf_reset, and vff_init_zero().

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ins_int_propagate()

void ins_int_propagate	(	struct Int32Vect3 *	accel,
		float	dt
	)

Definition at line 319 of file ins_int.c.

References ACCEL_BFP_OF_REAL, ACCEL_FLOAT_OF_BFP, hff_propagate(), ins_int, INS_MAX_PROPAGATION_STEPS, ins_ned_to_state(), ins_update_from_vff(), int32_rmat_transp_vmult(), InsInt::ltp_accel, InsInt::propagation_cnt, stateGetNedToBodyRMat_i(), stateSetAccelBody_i(), vff_propagate(), Int32Vect3::x, NedCoor_i::x, Int32Vect3::y, NedCoor_i::y, Int32Vect3::z, and NedCoor_i::z.

Referenced by accel_cb().

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ins_int_update_gps()

void ins_int_update_gps

(

struct GpsState *

gps_s

)

Todo:

maybe use gps_s->ned_vel directly??

Definition at line 422 of file ins_int.c.

References ecef_int_from_gps(), ecef_vel_int_from_gps(), GpsState::fix, GPS_FIX_3D, InsInt::hf_realign, hff_realign(), hff_update_gps(), ins_int, ins_ned_to_state(), 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, reset_ref(), stateGetNedToBodyQuat_i(), VECT2_ASSIGN, VECT2_SDIV, VECT3_SUB, vff_update_vz_conf(), vff_update_z_conf(), Int32Vect3::x, NedCoor_i::x, NedCoor_i::y, and NedCoor_i::z.

Referenced by gps_cb().

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Variable Documentation

ins_int

struct InsInt ins_int

extern

global INS state

Definition at line 168 of file ins_int.c.

Referenced by baro_cb(), ins_int_init(), ins_int_propagate(), ins_int_update_gps(), ins_ned_to_state(), ins_update_from_vff(), pos_est_cb(), reset_ref(), reset_vertical_pos(), reset_vertical_ref(), send_ins(), send_ins_ref(), send_ins_z(), and vel_est_cb().