Paparazzi UAS v7.0_unstable
Paparazzi is a free software Unmanned Aircraft System.
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mission_fw_nav.c
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1/*
2 * Copyright (C) 2013 Gautier Hattenberger
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 */
22
30#include <stdio.h>
32#include "autopilot.h"
35#include "generated/flight_plan.h"
36
39{
41 struct LlaCoor_f lla_f;
42 LLA_FLOAT_OF_BFP(lla_f, *lla);
43
44 /* Computes from (lat, long) in the referenced UTM zone */
45 struct UtmCoor_f utm;
47 utm_of_lla_f(&utm, &lla_f);
48
49 /* Computes relative position to HOME waypoint
50 * and bound the distance to max_dist_from_home
51 */
52 float dx, dy;
53 dx = utm.east - nav_utm_east0 - waypoints[WP_HOME].x;
54 dy = utm.north - nav_utm_north0 - waypoints[WP_HOME].y;
57
58 /* Update point */
59 point->x = waypoints[WP_HOME].x + dx;
60 point->y = waypoints[WP_HOME].y + dy;
61 point->z = lla_f.alt;
62
63 return true;
64}
65
66// navigation time step
67static const float dt_navigation = 1.0f / ((float)NAVIGATION_FREQUENCY);
68
69// dirty hack to comply with nav_approaching_xy function
70struct EnuCoor_f last_wp_f = { 0.f, 0.f, 0.f };
71
74static inline bool mission_nav_wp(struct _mission_wp *wp)
75{
79#endif
80 ) {
81 last_wp_f = wp->wp; // store last wp
82 return false; // end of mission element
83 }
84 // set navigation command
85 fly_to_xy(wp->wp.x, wp->wp.y);
88 return true;
89}
90
93static inline bool mission_nav_circle(struct _mission_circle *circle)
94{
95 nav_circle_XY(circle->center.x, circle->center.y, circle->radius);
97 NavVerticalAltitudeMode(circle->center.z, 0.f);
98 return true;
99}
100
104{
105 if (nav_approaching_xy(segment->to.x, segment->to.y, segment->from.x, segment->from.y, CARROT)
108#endif
109 ) {
110 last_wp_f = segment->to;
111 return false; // end of mission element
112 }
113 nav_route_xy(segment->from.x, segment->from.y, segment->to.x, segment->to.y);
115 NavVerticalAltitudeMode(segment->to.z, 0.f); // both altitude should be the same anyway
116 return true;
117}
118
121static inline bool mission_nav_path(struct _mission_path *path)
122{
123 if (path->nb == 0) {
124 return false; // nothing to do
125 }
126 if (path->nb == 1) {
127 // handle as a single waypoint
128 struct _mission_wp wp;
129 wp.wp = path->path[0];
130 return mission_nav_wp(&wp);
131 }
132 if (path->path_idx == path->nb - 1) {
133 last_wp_f = path->path[path->path_idx]; // store last wp
134 return false; // end of path
135 }
136 // normal case
137 struct EnuCoor_f from = path->path[path->path_idx];
138 struct EnuCoor_f to = path->path[path->path_idx + 1];
139 nav_route_xy(from.x, from.y, to.x, to.y);
141 NavVerticalAltitudeMode(to.z, 0.f); // both altitude should be the same anyway
142 if (nav_approaching_xy(to.x, to.y, from.x, from.y, CARROT)
145#endif
146 ) {
147 path->path_idx++; // go to next segment
148 }
149 return true;
150}
151
154static inline bool mission_nav_custom(struct _mission_custom *custom, bool init)
155{
156 if (init) {
157 return custom->reg->cb(custom->nb, custom->params, MissionInit);
158 } else {
159 return custom->reg->cb(custom->nb, custom->params, MissionRun);
160 }
161}
162
166#ifndef MISSION_WAIT_TIMEOUT
167#define MISSION_WAIT_TIMEOUT 120 // wait 2 minutes before ending mission
168#endif
169
170static bool mission_wait_started = false;
171#if MISSION_WAIT_TIMEOUT
172static float mission_wait_time = 0.f;
174static bool mission_wait_pattern(void) {
177 mission_wait_circle.center.z += GetAltRef();
179 mission_wait_time = 0.f;
181 }
184 return (mission_wait_time < (float)MISSION_WAIT_TIMEOUT); // keep flying until TIMEOUT
185}
186#else
187static bool mission_wait_pattern(void) {
188 return false; // no TIMEOUT, end mission now
189}
190#endif
191
193{
194 // current element
195 struct _mission_element *el = NULL;
196 if ((el = mission_get()) == NULL) {
197 return mission_wait_pattern();
198 }
199 mission_wait_started = false;
200
201 bool el_running = false;
202 switch (el->type) {
203 case MissionWP:
204 el_running = mission_nav_wp(&(el->element.mission_wp));
205 break;
206 case MissionCircle:
207 el_running = mission_nav_circle(&(el->element.mission_circle));
208 break;
209 case MissionSegment:
210 el_running = mission_nav_segment(&(el->element.mission_segment));
211 break;
212 case MissionPath:
213 el_running = mission_nav_path(&(el->element.mission_path));
214 break;
215 case MissionCustom:
216 el_running = mission_nav_custom(&(el->element.mission_custom), mission.element_time < dt_navigation);
217 break;
218 default:
219 // invalid type or pattern not yet handled
220 break;
221 }
222
223 // increment element_time
225
226 // test if element is finished or element time is elapsed
227 if (!el_running || (el->duration > 0.f && mission.element_time >= el->duration)) {
228 // reset timer
229 mission.element_time = 0.f;
230 // go to next element
232 }
233
234 return true;
235}
236
Core autopilot interface common to all firmwares.
int32_t nav_utm_east0
Definition common_nav.c:48
uint8_t nav_utm_zone0
Definition common_nav.c:50
struct point waypoints[NB_WAYPOINT]
size == nb_waypoint, waypoint 0 is a dummy waypoint
Definition common_nav.c:44
int32_t nav_utm_north0
Definition common_nav.c:49
float y
Definition common_nav.h:41
float x
Definition common_nav.h:40
#define LLA_FLOAT_OF_BFP(_o, _i)
vector in Latitude, Longitude and Altitude
static struct EnuCoor_f * stateGetPositionEnu_f(void)
Get position in local ENU coordinates (float).
Definition state.h:848
uint16_t foo
Definition main_demo5.c:58
struct _mission mission
struct _mission_element * mission_get(void)
Get current mission element.
mission planner library
struct EnuCoor_f wp
@ MissionCustom
@ MissionCircle
@ MissionWP
@ MissionSegment
@ MissionPath
@ MissionInit
first exec
@ MissionRun
normal run
float element_time
time in second spend in the current element
#define MISSION_ELEMENT_NB
Max number of elements in the tasks' list can be redefined.
struct EnuCoor_f center
struct EnuCoor_f path[MISSION_PATH_NB]
uint8_t current_idx
current mission element index
static bool mission_wait_pattern(void)
static bool mission_nav_wp(struct _mission_wp *wp)
Navigation function to a single waypoint.
static bool mission_nav_custom(struct _mission_custom *custom, bool init)
Call custom navigation function.
int mission_run()
Run mission.
bool mission_point_of_lla(struct EnuCoor_f *point, struct LlaCoor_i *lla)
Utility function: converts lla (int) to local point (float)
static bool mission_nav_circle(struct _mission_circle *circle)
Navigation function on a circle.
static const float dt_navigation
static bool mission_nav_path(struct _mission_path *path)
Navigation function along a path.
#define MISSION_WAIT_TIMEOUT
Implement waiting pattern Only called when MISSION_WAIT_TIMEOUT is not 0.
static bool mission_nav_segment(struct _mission_segment *segment)
Navigation function along a segment.
struct EnuCoor_f last_wp_f
static bool mission_wait_started
bool nav_approaching_xy(float x, float y, float from_x, float from_y, float approaching_time)
Decide if the UAV is approaching the current waypoint.
Definition nav.c:325
void nav_route_xy(float last_wp_x, float last_wp_y, float wp_x, float wp_y)
Computes the carrot position along the desired segment.
Definition nav.c:382
void nav_circle_XY(float x, float y, float radius)
Navigates around (x, y).
Definition nav.c:108
void fly_to_xy(float x, float y)
Computes desired_x, desired_y and desired_course.
Definition nav.c:356
Fixedwing Navigation library.
#define GetAltRef()
Get current altitude reference for local coordinates.
Definition nav.h:242
#define NAVIGATION_FREQUENCY
Default fixedwing navigation frequency.
Definition nav.h:49
#define NavVerticalAltitudeMode(_alt, _pre_climb)
Set the vertical mode to altitude control with the specified altitude setpoint and climb pre-command.
Definition nav.h:191
#define NavVerticalAutoThrottleMode(_pitch)
Set the climb control to auto-throttle with the specified pitch pre-command.
Definition nav.h:177
bool init
Definition nav_gls.c:57
void utm_of_lla_f(struct UtmCoor_f *utm, struct LlaCoor_f *lla)
float alt
in meters (normally above WGS84 reference ellipsoid)
float y
in meters
float x
in meters
uint8_t zone
UTM zone number.
float z
in meters
vector in East North Up coordinates Units: meters
vector in Latitude, Longitude and Altitude
position in UTM coordinates Units: meters
const float max_dist_from_home
Definition navigation.c:53
#define DEFAULT_CIRCLE_RADIUS
default nav_circle_radius in meters
Definition navigation.h:42
#define CARROT
default approaching_time for a wp
Definition navigation.h:70