Paparazzi UAS  v5.15_devel-81-gd13dafb
Paparazzi is a free software Unmanned Aircraft System.
 All Data Structures Namespaces Files Functions Variables Typedefs Enumerations Enumerator Macros Modules Pages
guidance_h.c
Go to the documentation of this file.
1 /*
2  * Copyright (C) 2017 Gautier Hattenberger <gautier.hattenberger@enac.fr>
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 
32 
34 {
36  h_ctl_course_loop(); /* aka compute nav_desired_roll */
37  }
38  // Copy the pitch setpoint from the guidance to the stabilization control
40 }
41 
void h_ctl_course_loop(void)
void h_ctl_guidance_loop(void)
General guidance logic This will call the proper control loops according to the sub-modes.
Definition: guidance_h.c:33
uint8_t lateral_mode
float v_ctl_pitch_setpoint
Definition: energy_ctrl.c:133
Fixed wing horizontal control.
#define LATERAL_MODE_COURSE
Vertical control for fixed wing vehicles.
Fixedwing specific autopilot interface and initialization.
Horizontal guidance logic for fixed wing vehicles.
float h_ctl_pitch_setpoint