Paparazzi UAS  v7.0_unstable
Paparazzi is a free software Unmanned Aircraft System.
ins_gps_passthrough.c
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1 /*
2  * Copyright (C) 2004-2012 The Paparazzi Team
3  *
4  * This file is part of paparazzi.
5  *
6  * paparazzi is free software; you can redistribute it and/or modify
7  * it under the terms of the GNU General Public License as published by
8  * the Free Software Foundation; either version 2, or (at your option)
9  * any later version.
10  *
11  * paparazzi is distributed in the hope that it will be useful,
12  * but WITHOUT ANY WARRANTY; without even the implied warranty of
13  * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
14  * GNU General Public License for more details.
15  *
16  * You should have received a copy of the GNU General Public License
17  * along with paparazzi; see the file COPYING. If not, write to
18  * the Free Software Foundation, 59 Temple Place - Suite 330,
19  * Boston, MA 02111-1307, USA.
20  */
21 
30 #include "modules/ins/ins.h"
31 
32 #include <inttypes.h>
33 #include <math.h>
34 
35 #include "state.h"
36 #include "modules/gps/gps.h"
37 #include "modules/core/abi.h"
38 
39 #ifndef USE_INS_NAV_INIT
40 #define USE_INS_NAV_INIT TRUE
41 PRINT_CONFIG_MSG("USE_INS_NAV_INIT defaulting to TRUE")
42 #endif
43 
44 #if USE_INS_NAV_INIT
45 #include "generated/flight_plan.h"
46 #endif
47 
48 
50  struct LtpDef_i ltp_def;
52 
53  /* output LTP NED */
54  struct NedCoor_i ltp_pos;
55  struct NedCoor_i ltp_speed;
56  struct NedCoor_i ltp_accel;
57 };
58 
60 
63 #ifndef INS_PT_IMU_ID
64 #define INS_PT_IMU_ID ABI_BROADCAST
65 #endif
67 static void accel_cb(uint8_t sender_id, uint32_t stamp, struct Int32Vect3 *accel);
68 
69 
73 #ifndef INS_PT_GPS_ID
74 #define INS_PT_GPS_ID GPS_MULTI_ID
75 #endif
78 
79 static void gps_cb(uint8_t sender_id __attribute__((unused)),
80  uint32_t stamp __attribute__((unused)),
81  struct GpsState *gps_s)
82 {
83  if (gps_s->fix < GPS_FIX_3D) {
84  return;
85  }
86  if (!ins_gp.ltp_initialized) {
88  }
89 
90  /* simply scale and copy pos/speed from gps */
91  struct NedCoor_i gps_pos_cm_ned;
92  struct EcefCoor_i ecef_pos = ecef_int_from_gps(gps_s);
93  ned_of_ecef_point_i(&gps_pos_cm_ned, &ins_gp.ltp_def, &ecef_pos);
94  INT32_VECT3_SCALE_2(ins_gp.ltp_pos, gps_pos_cm_ned,
97 
98  struct NedCoor_i gps_speed_cm_s_ned;
99  struct EcefCoor_i ecef_vel = ecef_vel_int_from_gps(gps_s);
100  ned_of_ecef_vect_i(&gps_speed_cm_s_ned, &ins_gp.ltp_def, &ecef_vel);
101  INT32_VECT3_SCALE_2(ins_gp.ltp_speed, gps_speed_cm_s_ned,
104 }
105 
106 
107 #if PERIODIC_TELEMETRY
109 
110 static void send_ins(struct transport_tx *trans, struct link_device *dev)
111 {
112  pprz_msg_send_INS(trans, dev, AC_ID,
116 }
117 
118 static void send_ins_z(struct transport_tx *trans, struct link_device *dev)
119 {
120  static float fake_baro_z = 0.0;
121  pprz_msg_send_INS_Z(trans, dev, AC_ID,
122  (float *)&fake_baro_z, &ins_gp.ltp_pos.z,
124 }
125 
126 static void send_ins_ref(struct transport_tx *trans, struct link_device *dev)
127 {
128  static float fake_qfe = 0.0;
129  if (ins_gp.ltp_initialized) {
130  pprz_msg_send_INS_REF(trans, dev, AC_ID,
133  &ins_gp.ltp_def.hmsl, (float *)&fake_qfe);
134  }
135 }
136 #endif
137 
139 {
140 
141 #if USE_INS_NAV_INIT
142  struct LlaCoor_i llh_nav0; /* Height above the ellipsoid */
143  llh_nav0.lat = NAV_LAT0;
144  llh_nav0.lon = NAV_LON0;
145  /* NAV_ALT0 = ground alt above msl, NAV_MSL0 = geoid-height (msl) over ellipsoid */
146  llh_nav0.alt = NAV_ALT0 + NAV_MSL0;
147 
148  struct EcefCoor_i ecef_nav0;
149  ecef_of_lla_i(&ecef_nav0, &llh_nav0);
150 
151  ltp_def_from_ecef_i(&ins_gp.ltp_def, &ecef_nav0);
152  ins_gp.ltp_def.hmsl = NAV_ALT0;
154 
155  ins_gp.ltp_initialized = true;
156 #else
157  ins_gp.ltp_initialized = false;
158 #endif
159 
163 
164 #if PERIODIC_TELEMETRY
168 #endif
169 
170  AbiBindMsgGPS(INS_PT_GPS_ID, &gps_ev, gps_cb);
171  AbiBindMsgIMU_ACCEL(INS_PT_IMU_ID, &accel_ev, accel_cb);
172 }
173 
175 {
176  struct EcefCoor_i ecef_pos = ecef_int_from_gps(&gps);
177  struct LlaCoor_i lla_pos = lla_int_from_gps(&gps);
178  ltp_def_from_ecef_i(&ins_gp.ltp_def, &ecef_pos);
179  ins_gp.ltp_def.lla.alt = lla_pos.alt;
182  ins_gp.ltp_initialized = true;
183 }
184 
186 {
187  struct LlaCoor_i lla = {
189  .lon = state.ned_origin_i.lla.lon,
190  .alt = gps.lla_pos.alt
191  };
195 }
196 
197 static void accel_cb(uint8_t sender_id __attribute__((unused)),
198  uint32_t stamp __attribute__((unused)),
199  struct Int32Vect3 *accel)
200 {
201  // untilt accel and remove gravity
202  struct Int32Vect3 accel_ned;
203  stateSetAccelBody_i(accel);
204  struct Int32RMat *ned_to_body_rmat = stateGetNedToBodyRMat_i();
205  int32_rmat_transp_vmult(&accel_ned, ned_to_body_rmat, accel);
206  accel_ned.z += ACCEL_BFP_OF_REAL(9.81);
207  stateSetAccelNed_i((struct NedCoor_i *)&accel_ned);
208  VECT3_COPY(ins_gp.ltp_accel, accel_ned);
209 }
Main include for ABI (AirBorneInterface).
Event structure to store callbacks in a linked list.
Definition: abi_common.h:67
struct GpsState gps
global GPS state
Definition: gps.c:69
struct LlaCoor_i lla_int_from_gps(struct GpsState *gps_s)
Get GPS lla (integer) Converted on the fly if not available.
Definition: gps.c:436
struct EcefCoor_i ecef_vel_int_from_gps(struct GpsState *gps_s)
Get GPS ecef velocity (integer) Converted on the fly if not available.
Definition: gps.c:494
struct EcefCoor_i ecef_int_from_gps(struct GpsState *gps_s)
Get GPS ecef pos (integer) Converted on the fly if not available.
Definition: gps.c:465
Device independent GPS code (interface)
int32_t hmsl
height above mean sea level (MSL) in mm
Definition: gps.h:93
struct LlaCoor_i lla_pos
position in LLA (lat,lon: deg*1e7; alt: mm over ellipsoid)
Definition: gps.h:91
#define GPS_FIX_3D
3D GPS fix
Definition: gps.h:43
data structure for GPS information
Definition: gps.h:86
#define VECT3_COPY(_a, _b)
Definition: pprz_algebra.h:140
#define INT32_POS_OF_CM_DEN
#define INT32_SPEED_OF_CM_S_NUM
#define ACCEL_BFP_OF_REAL(_af)
#define INT32_SPEED_OF_CM_S_DEN
#define INT32_POS_OF_CM_NUM
#define INT32_VECT3_ZERO(_v)
void int32_rmat_transp_vmult(struct Int32Vect3 *vb, struct Int32RMat *m_b2a, struct Int32Vect3 *va)
rotate 3D vector by transposed rotation matrix.
#define INT32_VECT3_SCALE_2(_a, _b, _num, _den)
rotation matrix
int32_t lat
in degrees*1e7
int32_t hmsl
Height above mean sea level in mm.
int32_t alt
in millimeters above WGS84 reference ellipsoid
int32_t z
Down.
int32_t z
in centimeters
struct LlaCoor_i lla
Reference point in lla.
int32_t x
in centimeters
int32_t y
East.
struct EcefCoor_i ecef
Reference point in ecef.
int32_t y
in centimeters
int32_t lon
in degrees*1e7
int32_t x
North.
void ecef_of_lla_i(struct EcefCoor_i *out, struct LlaCoor_i *in)
Convert a LLA to ECEF.
void ltp_def_from_ecef_i(struct LtpDef_i *def, struct EcefCoor_i *ecef)
void ned_of_ecef_point_i(struct NedCoor_i *ned, struct LtpDef_i *def, struct EcefCoor_i *ecef)
Convert a point from ECEF to local NED.
void ned_of_ecef_vect_i(struct NedCoor_i *ned, struct LtpDef_i *def, struct EcefCoor_i *ecef)
Rotate a vector from ECEF to NED.
void ltp_def_from_lla_i(struct LtpDef_i *def, struct LlaCoor_i *lla)
vector in EarthCenteredEarthFixed coordinates
vector in Latitude, Longitude and Altitude
definition of the local (flat earth) coordinate system
vector in North East Down coordinates
static void stateSetAccelNed_i(struct NedCoor_i *ned_accel)
Set acceleration in NED coordinates (int).
Definition: state.h:986
static struct Int32RMat * stateGetNedToBodyRMat_i(void)
Get vehicle body attitude rotation matrix (int).
Definition: state.h:1119
struct State state
Definition: state.c:36
struct LtpDef_i ned_origin_i
Definition of the local (flat earth) coordinate system.
Definition: state.h:166
static void stateSetPositionNed_i(struct NedCoor_i *ned_pos)
Set position from local NED coordinates (int).
Definition: state.h:531
static void stateSetLocalOrigin_i(struct LtpDef_i *ltp_def)
Set the local (flat earth) coordinate frame origin (int).
Definition: state.h:457
static void stateSetAccelBody_i(struct Int32Vect3 *body_accel)
Set acceleration in Body coordinates (int).
Definition: state.h:855
static void stateSetSpeedNed_i(struct NedCoor_i *ned_speed)
Set ground speed in local NED coordinates (int).
Definition: state.h:763
Integrated Navigation System interface.
void ins_reset_local_origin(void)
INS local origin reset.
static void gps_cb(uint8_t sender_id, uint32_t stamp, struct GpsState *gps_s)
struct NedCoor_i ltp_speed
static void send_ins(struct transport_tx *trans, struct link_device *dev)
struct InsGpsPassthrough ins_gp
struct NedCoor_i ltp_accel
static abi_event accel_ev
void ins_gps_passthrough_init(void)
static void send_ins_ref(struct transport_tx *trans, struct link_device *dev)
static void send_ins_z(struct transport_tx *trans, struct link_device *dev)
#define INS_PT_IMU_ID
ABI bindings on ACCEL data.
struct LtpDef_i ltp_def
void ins_reset_altitude_ref(void)
INS altitude reference reset.
static void accel_cb(uint8_t sender_id, uint32_t stamp, struct Int32Vect3 *accel)
#define INS_PT_GPS_ID
ABI binding for gps data.
struct NedCoor_i ltp_pos
static abi_event gps_ev
Simply passes GPS through to the state interface.
PRINT_CONFIG_MSG("USE_INS_NAV_INIT defaulting to TRUE")
PRINT_CONFIG_VAR(ONELOOP_ANDI_FILT_CUTOFF)
API to get/set the generic vehicle states.
static const struct usb_device_descriptor dev
Definition: usb_ser_hw.c:74
int8_t register_periodic_telemetry(struct periodic_telemetry *_pt, uint8_t _id, telemetry_cb _cb)
Register a telemetry callback function.
Definition: telemetry.c:51
Periodic telemetry system header (includes downlink utility and generated code).
#define DefaultPeriodic
Set default periodic telemetry.
Definition: telemetry.h:66
unsigned int uint32_t
Typedef defining 32 bit unsigned int type.
Definition: vl53l1_types.h:78
unsigned char uint8_t
Typedef defining 8 bit unsigned char type.
Definition: vl53l1_types.h:98