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 
71 static void reset_cb(uint8_t sender_id, uint8_t flag);
72 
76 #ifndef INS_PT_GPS_ID
77 #define INS_PT_GPS_ID GPS_MULTI_ID
78 #endif
81 
82 static void gps_cb(uint8_t sender_id __attribute__((unused)),
83  uint32_t stamp __attribute__((unused)),
84  struct GpsState *gps_s)
85 {
86  if (gps_s->fix < GPS_FIX_3D) {
87  return;
88  }
89  if (!ins_gp.ltp_initialized) {
90  reset_cb(MODULE_INS_GPS_PASSTHROUGH_ID, INS_RESET_REF);
91  }
92 
93  /* simply scale and copy pos/speed from gps */
94  struct NedCoor_i gps_pos_cm_ned;
95  struct EcefCoor_i ecef_pos = ecef_int_from_gps(gps_s);
96  ned_of_ecef_point_i(&gps_pos_cm_ned, &ins_gp.ltp_def, &ecef_pos);
97  INT32_VECT3_SCALE_2(ins_gp.ltp_pos, gps_pos_cm_ned,
99  stateSetPositionNed_i(MODULE_INS_GPS_PASSTHROUGH_ID, &ins_gp.ltp_pos);
100 
101  struct NedCoor_i gps_speed_cm_s_ned;
102  struct EcefCoor_i ecef_vel = ecef_vel_int_from_gps(gps_s);
103  ned_of_ecef_vect_i(&gps_speed_cm_s_ned, &ins_gp.ltp_def, &ecef_vel);
104  INT32_VECT3_SCALE_2(ins_gp.ltp_speed, gps_speed_cm_s_ned,
106  stateSetSpeedNed_i(MODULE_INS_GPS_PASSTHROUGH_ID, &ins_gp.ltp_speed);
107 }
108 
109 
110 #if PERIODIC_TELEMETRY
112 
113 static void send_ins(struct transport_tx *trans, struct link_device *dev)
114 {
115  pprz_msg_send_INS(trans, dev, AC_ID,
119 }
120 
121 static void send_ins_z(struct transport_tx *trans, struct link_device *dev)
122 {
123  static float fake_baro_z = 0.0;
124  pprz_msg_send_INS_Z(trans, dev, AC_ID,
125  (float *)&fake_baro_z, &ins_gp.ltp_pos.z,
127 }
128 
129 static void send_ins_ref(struct transport_tx *trans, struct link_device *dev)
130 {
131  static float fake_qfe = 0.0;
132  if (ins_gp.ltp_initialized) {
133  pprz_msg_send_INS_REF(trans, dev, AC_ID,
136  &ins_gp.ltp_def.hmsl, (float *)&fake_qfe);
137  }
138 }
139 #endif
140 
142 {
143 
144 #if USE_INS_NAV_INIT
145  struct LlaCoor_i llh_nav0; /* Height above the ellipsoid */
146  llh_nav0.lat = NAV_LAT0;
147  llh_nav0.lon = NAV_LON0;
148  /* NAV_ALT0 = ground alt above msl, NAV_MSL0 = geoid-height (msl) over ellipsoid */
149  llh_nav0.alt = NAV_ALT0 + NAV_MSL0;
150 
151  struct EcefCoor_i ecef_nav0;
152  ecef_of_lla_i(&ecef_nav0, &llh_nav0);
153 
154  ltp_def_from_ecef_i(&ins_gp.ltp_def, &ecef_nav0);
155  ins_gp.ltp_def.hmsl = NAV_ALT0;
156  stateSetLocalOrigin_i(MODULE_INS_GPS_PASSTHROUGH_ID, &ins_gp.ltp_def);
157 
158  ins_gp.ltp_initialized = true;
159 #else
160  ins_gp.ltp_initialized = false;
161 #endif
162 
166 
167 #if PERIODIC_TELEMETRY
171 #endif
172 
173  AbiBindMsgGPS(INS_PT_GPS_ID, &gps_ev, gps_cb);
174  AbiBindMsgIMU_ACCEL(INS_PT_IMU_ID, &accel_ev, accel_cb);
175  AbiBindMsgINS_RESET(ABI_BROADCAST, &reset_ev, reset_cb);
176 }
177 
178 static void reset_ref(void)
179 {
180  struct EcefCoor_i ecef_pos = ecef_int_from_gps(&gps);
181  struct LlaCoor_i lla_pos = lla_int_from_gps(&gps);
182  ltp_def_from_ecef_i(&ins_gp.ltp_def, &ecef_pos);
183  ins_gp.ltp_def.lla.alt = lla_pos.alt;
185  stateSetLocalOrigin_i(MODULE_INS_GPS_PASSTHROUGH_ID, &ins_gp.ltp_def);
186  ins_gp.ltp_initialized = true;
187 }
188 
189 static void reset_vertical_ref(void)
190 {
191  struct LlaCoor_i lla = {
193  .lon = stateGetLlaOrigin_i().lon,
194  .alt = gps.lla_pos.alt
195  };
198  stateSetLocalOrigin_i(MODULE_INS_GPS_PASSTHROUGH_ID, &ins_gp.ltp_def);
199 }
200 
201 static void reset_cb(uint8_t sender_id UNUSED, uint8_t flag)
202 {
203  switch (flag) {
204  case INS_RESET_REF:
205  reset_ref();
206  break;
209  break;
210  default:
211  // unsupported cases
212  break;
213  }
214 }
215 
216 static void accel_cb(uint8_t sender_id __attribute__((unused)),
217  uint32_t stamp __attribute__((unused)),
218  struct Int32Vect3 *accel)
219 {
220  // untilt accel and remove gravity
221  struct Int32Vect3 accel_ned;
222  stateSetAccelBody_i(MODULE_INS_GPS_PASSTHROUGH_ID, accel);
223  struct Int32RMat *ned_to_body_rmat = stateGetNedToBodyRMat_i();
224  int32_rmat_transp_vmult(&accel_ned, ned_to_body_rmat, accel);
225  accel_ned.z += ACCEL_BFP_OF_REAL(9.81);
226  stateSetAccelNed_i(MODULE_INS_GPS_PASSTHROUGH_ID, (struct NedCoor_i *)&accel_ned);
227  VECT3_COPY(ins_gp.ltp_accel, accel_ned);
228 }
Main include for ABI (AirBorneInterface).
#define ABI_BROADCAST
Broadcast address.
Definition: abi_common.h:58
Event structure to store callbacks in a linked list.
Definition: abi_common.h:67
uint8_t last_wp UNUSED
struct GpsState gps
global GPS state
Definition: gps.c:74
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:464
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:522
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:493
Device independent GPS code (interface)
int32_t hmsl
height above mean sea level (MSL) in mm
Definition: gps.h:94
struct LlaCoor_i lla_pos
position in LLA (lat,lon: deg*1e7; alt: mm over ellipsoid)
Definition: gps.h:92
#define GPS_FIX_3D
3D GPS fix
Definition: gps.h:44
data structure for GPS information
Definition: gps.h:87
#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(uint16_t id, struct NedCoor_i *ned_accel)
Set acceleration in NED coordinates (int).
Definition: state.h:1127
static void stateSetAccelBody_i(uint16_t id, struct Int32Vect3 *body_accel)
Set acceleration in Body coordinates (int).
Definition: state.h:1167
static struct Int32RMat * stateGetNedToBodyRMat_i(void)
Get vehicle body attitude rotation matrix (int).
Definition: state.h:1282
static void stateSetLocalOrigin_i(uint16_t id, struct LtpDef_i *ltp_def)
Set the local (flat earth) coordinate frame origin (int).
Definition: state.h:519
struct LlaCoor_i stateGetLlaOrigin_i(void)
Get the LLA position of the frame origin (int)
Definition: state.c:124
static void stateSetPositionNed_i(uint16_t id, struct NedCoor_i *ned_pos)
Set position from local NED coordinates (int).
Definition: state.h:638
static void stateSetSpeedNed_i(uint16_t id, struct NedCoor_i *ned_speed)
Set ground speed in local NED coordinates (int).
Definition: state.h:892
Integrated Navigation System interface.
#define INS_RESET_VERTICAL_REF
Definition: ins.h:37
#define INS_RESET_REF
flags for INS reset
Definition: ins.h:36
static void reset_vertical_ref(void)
static void gps_cb(uint8_t sender_id, uint32_t stamp, struct GpsState *gps_s)
struct NedCoor_i ltp_speed
static void reset_cb(uint8_t sender_id, uint8_t flag)
static void send_ins(struct transport_tx *trans, struct link_device *dev)
struct InsGpsPassthrough ins_gp
struct NedCoor_i ltp_accel
static void reset_ref(void)
static abi_event accel_ev
static abi_event reset_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
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