Paparazzi UAS v7.0_unstable
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ahrs_float_cmpl_wrapper.c
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1/*
2 * Copyright (C) 2015 Felix Ruess <felix.ruess@gmail.com>
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, see
18 * <http://www.gnu.org/licenses/>.
19 */
20
28#include "modules/ahrs/ahrs.h"
29#include "modules/core/abi.h"
30#include "state.h"
31
33
34
36
39
41
42#if PERIODIC_TELEMETRY
44#include "mcu_periph/sys_time.h"
45#include "state.h"
46
47static void send_euler(struct transport_tx *trans, struct link_device *dev)
48{
49 struct FloatEulers ltp_to_body_euler;
50 float_eulers_of_quat(&ltp_to_body_euler, &ahrs_fc.ltp_to_body_quat);
52 &ltp_to_body_euler.phi,
53 &ltp_to_body_euler.theta,
54 &ltp_to_body_euler.psi,
55 &ahrs_fc_id);
56}
57
58static void send_bias(struct transport_tx *trans, struct link_device *dev)
59{
60 struct Int32Rates gyro_bias;
63 &gyro_bias.p, &gyro_bias.q, &gyro_bias.r, &ahrs_fc_id);
64}
65
66static void send_euler_int(struct transport_tx *trans, struct link_device *dev)
67{
68 /* compute eulers in int (IMU frame) */
69 struct FloatEulers ltp_to_body_euler;
70 float_eulers_of_quat(&ltp_to_body_euler, &ahrs_fc.ltp_to_body_quat);
72 EULERS_BFP_OF_REAL(eulers_body, ltp_to_body_euler);
73
75 &eulers_body.phi,
76 &eulers_body.theta,
77 &eulers_body.psi,
78 &eulers_body.phi,
79 &eulers_body.theta,
80 &eulers_body.psi,
81 &ahrs_fc_id);
82}
83
84static void send_geo_mag(struct transport_tx *trans, struct link_device *dev)
85{
88}
89
90static void send_filter_status(struct transport_tx *trans, struct link_device *dev)
91{
92 uint8_t mde = 3;
93 uint16_t val = 0;
94 if (!ahrs_fc.is_aligned) { mde = 2; }
96 /* set lost if no new gyro measurements for 50ms */
97 if (t_diff > 50000) { mde = 5; }
99}
100#endif
101
102
106#ifndef AHRS_FC_IMU_ID
107#define AHRS_FC_IMU_ID ABI_BROADCAST
108#endif
113#ifndef AHRS_FC_MAG_ID
114#define AHRS_FC_MAG_ID AHRS_FC_IMU_ID
115#endif
120#ifndef AHRS_FC_GPS_ID
121#define AHRS_FC_GPS_ID GPS_MULTI_ID
122#endif
130
131
133 uint32_t stamp, struct Int32Rates *gyro)
134{
136 struct FloatRates gyro_f;
138
139#if USE_AUTO_AHRS_FREQ || !defined(AHRS_PROPAGATE_FREQUENCY)
140 PRINT_CONFIG_MSG("Calculating dt for AHRS_FC propagation.")
141 /* timestamp in usec when last callback was received */
142 static uint32_t last_stamp = 0;
143
144 if (last_stamp > 0 && ahrs_fc.is_aligned) {
145 float dt = (float)(stamp - last_stamp) * 1e-6;
148 }
149 last_stamp = stamp;
150#else
151 PRINT_CONFIG_MSG("Using fixed AHRS_PROPAGATE_FREQUENCY for AHRS_FC propagation.")
154 const float dt = 1. / (AHRS_PROPAGATE_FREQUENCY);
157 }
158#endif
159}
160
162 uint32_t __attribute__((unused)) stamp,
163 struct Int32Vect3 *accel)
164{
165 struct FloatVect3 accel_f;
167
168#if USE_AUTO_AHRS_FREQ || !defined(AHRS_CORRECT_FREQUENCY)
169 PRINT_CONFIG_MSG("Calculating dt for AHRS float_cmpl accel update.")
170 static uint32_t last_stamp = 0;
171 if (last_stamp > 0 && ahrs_fc.is_aligned) {
172 float dt = (float)(stamp - last_stamp) * 1e-6;
174 }
175 last_stamp = stamp;
176#else
177 PRINT_CONFIG_MSG("Using fixed AHRS_CORRECT_FREQUENCY for AHRS float_cmpl accel update.")
179 if (ahrs_fc.is_aligned) {
180 const float dt = 1. / (AHRS_CORRECT_FREQUENCY);
182 }
183#endif
184}
185
186static void mag_cb(uint8_t __attribute__((unused)) sender_id,
187 uint32_t __attribute__((unused)) stamp,
188 struct Int32Vect3 *mag)
189{
190 struct FloatVect3 mag_f;
192
193#if USE_AUTO_AHRS_FREQ || !defined(AHRS_MAG_CORRECT_FREQUENCY)
194 PRINT_CONFIG_MSG("Calculating dt for AHRS float_cmpl mag update.")
195 static uint32_t last_stamp = 0;
196 if (last_stamp > 0 && ahrs_fc.is_aligned) {
197 float dt = (float)(stamp - last_stamp) * 1e-6;
199 }
200 last_stamp = stamp;
201#else
202 PRINT_CONFIG_MSG("Using fixed AHRS_MAG_CORRECT_FREQUENCY for AHRS float_cmpl mag update.")
204 if (ahrs_fc.is_aligned) {
205 const float dt = 1. / (AHRS_MAG_CORRECT_FREQUENCY);
207 }
208#endif
209}
210
212 uint32_t stamp __attribute__((unused)),
213 struct Int32Rates *lp_gyro, struct Int32Vect3 *lp_accel,
214 struct Int32Vect3 *lp_mag)
215{
216 if (!ahrs_fc.is_aligned) {
217 /* convert to float */
218 struct FloatRates gyro_f;
219 RATES_FLOAT_OF_BFP(gyro_f, *lp_gyro);
220 struct FloatVect3 accel_f;
221 ACCELS_FLOAT_OF_BFP(accel_f, *lp_accel);
222 struct FloatVect3 mag_f;
223 MAGS_FLOAT_OF_BFP(mag_f, *lp_mag);
224 /* use low passed values to align */
225 if (ahrs_fc_align(&gyro_f, &accel_f, &mag_f)) {
227 }
228 }
229}
230
231static void geo_mag_cb(uint8_t sender_id __attribute__((unused)), struct FloatVect3 *h)
232{
233 ahrs_fc.mag_h = *h;
234}
235
243
247#if (defined MODULE_AHRS_FLOAT_CMPL_QUAT_ID)
248#define MODULE_AHRS_FLOAT_CMPL_ID MODULE_AHRS_FLOAT_CMPL_QUAT_ID
249#elif (defined MODULE_AHRS_FLOAT_CMPL_RMAT_ID)
250#define MODULE_AHRS_FLOAT_CMPL_ID MODULE_AHRS_FLOAT_CMPL_RMAT_ID
251#else
252#error "wrong ahrs_cmpl module type"
253#endif
259
287
296
static void h(const real32_T x[7], const real32_T q[4], real32_T y[6])
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
#define AHRS_COMP_ID_FC
Definition ahrs.h:40
#define AHRS_PRIMARY
Definition ahrs.h:32
struct AhrsFloatCmpl ahrs_fc
void ahrs_fc_init(void)
void ahrs_fc_update_mag(struct FloatVect3 *mag, float dt)
bool ahrs_fc_align(struct FloatRates *lp_gyro, struct FloatVect3 *lp_accel, struct FloatVect3 *lp_mag)
void ahrs_fc_propagate(struct FloatRates *gyro, float dt)
void ahrs_fc_update_accel(struct FloatVect3 *accel, float dt)
void ahrs_fc_update_gps(struct GpsState *gps_s)
struct FloatRates gyro_bias
struct FloatRates body_rate
@ AHRS_FC_RUNNING
enum AhrsFCStatus status
struct FloatVect3 mag_h
struct FloatQuat ltp_to_body_quat
static uint8_t ahrs_fc_id
uint8_t ahrs_fc_enable
if TRUE with push the estimation results to the state interface
static void gps_cb(uint8_t sender_id, uint32_t stamp, struct GpsState *gps_s)
static void compute_body_orientation_and_rates(void)
Compute body orientation and rates from imu orientation and rates.
static abi_event mag_ev
static abi_event accel_ev
static void gyro_cb(uint8_t sender_id, uint32_t stamp, struct Int32Rates *gyro)
static void mag_cb(uint8_t sender_id, uint32_t stamp, struct Int32Vect3 *mag)
#define AHRS_FC_MAG_ID
ABI binding for magnetometer data.
void ahrs_fc_wrapper_init(void)
static abi_event gyro_ev
#define AHRS_FC_IMU_ID
ABI binding for IMU data.
static void send_geo_mag(struct transport_tx *trans, struct link_device *dev)
static abi_event aligner_ev
static abi_event geo_mag_ev
static void send_filter_status(struct transport_tx *trans, struct link_device *dev)
static void send_euler_int(struct transport_tx *trans, struct link_device *dev)
static void accel_cb(uint8_t sender_id, uint32_t stamp, struct Int32Vect3 *accel)
static void geo_mag_cb(uint8_t sender_id, struct FloatVect3 *h)
static void aligner_cb(uint8_t sender_id, uint32_t stamp, struct Int32Rates *lp_gyro, struct Int32Vect3 *lp_accel, struct Int32Vect3 *lp_mag)
static void send_euler(struct transport_tx *trans, struct link_device *dev)
static uint32_t ahrs_fc_last_stamp
void ahrs_float_cmpl_wrapper_enable(uint8_t enable)
static void send_bias(struct transport_tx *trans, struct link_device *dev)
#define AHRS_FC_GPS_ID
ABI binding for gps data.
static abi_event gps_ev
Paparazzi specific wrapper to run floating point complementary filter.
uint32_t get_sys_time_usec(void)
Get the time in microseconds since startup.
data structure for GPS information
Definition gps.h:87
#define STATE_INPUT_RATES
Definition state.h:145
#define STATE_INPUT_ATTITUDE
Definition state.h:144
float phi
in radians
float theta
in radians
float psi
in radians
void float_eulers_of_quat(struct FloatEulers *e, struct FloatQuat *q)
euler rotation 'ZYX'
euler angles
angular rates
#define MAGS_FLOAT_OF_BFP(_ef, _ei)
#define EULERS_BFP_OF_REAL(_ei, _ef)
#define RATES_BFP_OF_REAL(_ri, _rf)
#define RATES_FLOAT_OF_BFP(_rf, _ri)
#define ACCELS_FLOAT_OF_BFP(_ef, _ei)
int32_t p
in rad/s with INT32_RATE_FRAC
int32_t r
in rad/s with INT32_RATE_FRAC
int32_t q
in rad/s with INT32_RATE_FRAC
euler angles
angular rates
static void stateSetNedToBodyQuat_f(uint16_t id, struct FloatQuat *ned_to_body_quat)
Set vehicle body attitude from quaternion (float).
Definition state.h:1253
void stateSetInputFilter(uint8_t type, uint16_t flag)
set the input filter for a specified type of data.
Definition state.c:85
static void stateSetBodyRates_f(uint16_t id, struct FloatRates *body_rate)
Set vehicle body angular rate (float).
Definition state.h:1346
#define AHRS_PROPAGATE_FREQUENCY
Definition hf_float.c:55
PRINT_CONFIG_MSG("USE_INS_NAV_INIT defaulting to TRUE")
uint16_t foo
Definition main_demo5.c:58
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
Architecture independent timing functions.
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
uint16_t val[TCOUPLE_NB]
unsigned short uint16_t
Typedef defining 16 bit unsigned short type.
unsigned int uint32_t
Typedef defining 32 bit unsigned int type.
unsigned char uint8_t
Typedef defining 8 bit unsigned char type.