Paparazzi UAS v7.0_unstable
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ahrs_int_cmpl_quat.h
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1/*
2 * Copyright (C) 2008-2013 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,
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20 */
21
31#ifndef AHRS_INT_CMPL_QUAT_H
32#define AHRS_INT_CMPL_QUAT_H
33
34#include "modules/ahrs/ahrs.h"
35#include "modules/gps/gps.h"
36#include "std.h"
39
44
56
60 float weight;
63 float mag_kp;
64 float mag_ki;
65
66 /* parameters/options that can be changed */
69
74
80
86
90 float mag_omega;
91
95 float mag_zeta;
96
97 /* internal counters for the gains */
100
103};
104
105extern struct AhrsIntCmplQuat ahrs_icq;
106
107extern void ahrs_icq_init(void);
108extern bool ahrs_icq_align(struct Int32Rates *lp_gyro, struct Int32Vect3 *lp_accel,
109 struct Int32Vect3 *lp_mag);
110extern void ahrs_icq_propagate(struct Int32Rates *gyro, float dt);
111extern void ahrs_icq_update_accel(struct Int32Vect3 *accel, float dt);
112extern void ahrs_icq_update_mag(struct Int32Vect3 *mag, float dt);
113extern void ahrs_icq_update_gps(struct GpsState *gps_s);
114
120
127
128
130extern void ahrs_icq_set_accel_gains(void);
131
132static inline void ahrs_int_cmpl_quat_SetAccelOmega(float omega)
133{
134 ahrs_icq.accel_omega = omega;
136}
137
138static inline void ahrs_int_cmpl_quat_SetAccelZeta(float zeta)
139{
140 ahrs_icq.accel_zeta = zeta;
142}
143
145extern void ahrs_icq_set_mag_gains(void);
146
147static inline void ahrs_int_cmpl_quat_SetMagOmega(float omega)
148{
149 ahrs_icq.mag_omega = omega;
151}
152
153static inline void ahrs_int_cmpl_quat_SetMagZeta(float zeta)
154{
155 ahrs_icq.mag_zeta = zeta;
157}
158
159
160#endif /* AHRS_INT_CMPL_QUAT_H */
bool ahrs_icq_align(struct Int32Rates *lp_gyro, struct Int32Vect3 *lp_accel, struct Int32Vect3 *lp_mag)
uint16_t accel_cnt
number of propagations since last accel update
struct Int32Rates gyro_bias
AhrsICQStatus
@ AHRS_ICQ_UNINIT
@ AHRS_ICQ_RUNNING
void ahrs_icq_update_accel(struct Int32Vect3 *accel, float dt)
uint16_t mag_cnt
number of propagations since last mag update
struct Int32Vect3 mag_h
float mag_omega
filter cut-off frequency for correcting the attitude (heading) from magnetometer.
uint8_t gravity_heuristic_factor
sets how strongly the gravity heuristic reduces accel correction.
struct AhrsIntCmplQuat ahrs_icq
Default Rate filter Low pass.
struct Int32Rates rate_correction
float mag_zeta
filter damping for correcting the gyro bias from magnetometer.
static void ahrs_int_cmpl_quat_SetAccelOmega(float omega)
void ahrs_icq_init(void)
void ahrs_icq_update_gps(struct GpsState *gps_s)
struct Int64Rates high_rez_bias
void ahrs_icq_update_heading(int32_t heading)
Update yaw based on a heading measurement.
float accel_omega
filter cut-off frequency for correcting the attitude from accels.
void ahrs_icq_realign_heading(int32_t heading)
Hard reset yaw to a heading.
struct Int32Rates body_rate
void ahrs_icq_update_mag(struct Int32Vect3 *mag, float dt)
static void ahrs_int_cmpl_quat_SetAccelZeta(float zeta)
struct Int32Quat ltp_to_body_quat
static void ahrs_int_cmpl_quat_SetMagZeta(float zeta)
void ahrs_icq_set_accel_gains(void)
update pre-computed inv_kp and inv_ki gains from acc_omega and acc_zeta
struct Int64Quat high_rez_quat
void ahrs_icq_set_mag_gains(void)
update pre-computed kp and ki gains from mag_omega and mag_zeta
enum AhrsICQStatus status
status of the AHRS, AHRS_ICQ_UNINIT or AHRS_ICQ_RUNNING
static void ahrs_int_cmpl_quat_SetMagOmega(float omega)
void ahrs_icq_propagate(struct Int32Rates *gyro, float dt)
bool correct_gravity
enable gravity vector correction by removing centrifugal acceleration
float accel_zeta
filter damping for correcting the gyro-bias from accels.
Ahrs implementation specifc values.
Device independent GPS code (interface)
data structure for GPS information
Definition gps.h:87
Rotation quaternion.
angular rates
uint16_t foo
Definition main_demo5.c:58
Paparazzi fixed point algebra.
Generic orientation representation and conversions.
unsigned short uint16_t
Typedef defining 16 bit unsigned short type.
int int32_t
Typedef defining 32 bit int type.
unsigned char uint8_t
Typedef defining 8 bit unsigned char type.
float heading
Definition wedgebug.c:258