Paparazzi UAS  v5.18.0_stable
Paparazzi is a free software Unmanned Aircraft System.
guidance_indi_hybrid.h
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1 /*
2  * Copyright (C) 2015 Ewoud Smeur <ewoud.smeur@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, write to
18  * the Free Software Foundation, 59 Temple Place - Suite 330,
19  * Boston, MA 02111-1307, USA.
20  */
21 
30 #ifndef GUIDANCE_INDI_HYBRID_H
31 #define GUIDANCE_INDI_HYBRID_H
32 
33 #include "std.h"
34 #include "math/pprz_algebra_int.h"
37 
38 extern void guidance_indi_enter(void);
39 extern void guidance_indi_run(float *heading_sp);
40 extern void stabilization_attitude_set_setpoint_rp_quat_f(struct FloatEulers* indi_rp_cmd, bool in_flight, int32_t heading);
41 extern void guidance_indi_init(void);
42 extern void guidance_indi_propagate_filters(void);
43 
45  float pos_gain;
46  float pos_gainz;
47  float speed_gain;
48  float speed_gainz;
49 };
50 
52 
53 #endif /* GUIDANCE_INDI_HYBRID_H */
pprz_algebra_float.h
Paparazzi floating point algebra.
pprz_algebra_int.h
Paparazzi fixed point algebra.
gih_params
struct guidance_indi_hybrid_params gih_params
Definition: guidance_indi_hybrid.c:64
std.h
guidance_indi_enter
void guidance_indi_enter(void)
Call upon entering indi guidance.
Definition: guidance_indi.c:134
guidance_indi_init
void guidance_indi_init(void)
Init function.
Definition: guidance_indi.c:125
stabilization_attitude_set_setpoint_rp_quat_f
void stabilization_attitude_set_setpoint_rp_quat_f(struct FloatEulers *indi_rp_cmd, bool in_flight, int32_t heading)
guidance_indi_hybrid_params::speed_gainz
float speed_gainz
Definition: guidance_indi_hybrid.h:48
guidance_indi_run
void guidance_indi_run(float *heading_sp)
Definition: guidance_indi.c:154
guidance_indi_hybrid_params::pos_gainz
float pos_gainz
Definition: guidance_indi_hybrid.h:46
guidance_indi_hybrid_params::pos_gain
float pos_gain
Definition: guidance_indi_hybrid.h:45
int32_t
signed long int32_t
Definition: types.h:19
guidance_indi_propagate_filters
void guidance_indi_propagate_filters(void)
Low pass the accelerometer measurements to remove noise from vibrations.
Definition: guidance_indi_hybrid.c:420
guidance_indi_hybrid_params
Definition: guidance_indi_hybrid.h:44
FloatEulers
euler angles
Definition: pprz_algebra_float.h:84
guidance_indi_hybrid_params::speed_gain
float speed_gain
Definition: guidance_indi_hybrid.h:47
high_pass_filter.h
Simple high pass filter with double precision.
heading
float heading
Definition: wedgebug.c:258