Paparazzi UAS v7.0_unstable
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nav_survey_polygon_gvf.c
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1/*
2 * Copyright (C) 2017 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,
19 * Boston, MA 02111-1307, USA.
20 */
21
31#include "state.h"
32#include "autopilot.h"
33#include "generated/flight_plan.h"
35
36#ifdef DIGITAL_CAM
38#endif
39
41
42static void gvf_nav_points(struct FloatVect2 start, struct FloatVect2 end)
43{
44 gvf_segment_XY1_XY2(start.x, start.y, end.x, end.y);
45}
46
55static bool gvf_intercept_two_lines(struct FloatVect2 *p, struct FloatVect2 x, struct FloatVect2 y, float a1, float a2,
56 float b1, float b2)
57{
58 float divider, fac;
59
60 divider = (((b2 - a2) * (y.x - x.x)) + ((x.y - y.y) * (b1 - a1)));
61 if (divider == 0) { return false; }
62 fac = ((y.x * (x.y - a2)) + (x.x * (a2 - y.y)) + (a1 * (y.y - x.y))) / divider;
63 if (fac > 1.0) { return false; }
64 if (fac < 0.0) { return false; }
65
66 p->x = a1 + fac * (b1 - a1);
67 p->y = a2 + fac * (b2 - a2);
68
69 return true;
70}
71
78static bool gvf_get_two_intersects(struct FloatVect2 *x, struct FloatVect2 *y, struct FloatVect2 a, struct FloatVect2 b)
79{
80 int i, count = 0;
81 struct FloatVect2 tmp;
82
83 for (i = 0; i < gvf_survey.poly_count - 1; i++)
86 if (count == 0) {
87 *x = tmp;
88 count++;
89 } else {
90 *y = tmp;
91 count++;
92 break;
93 }
94 }
95
96 //wrapover first,last polygon waypoint
97 if (count == 1
101 *y = tmp;
102 count++;
103 }
104
105 if (count != 2) {
106 return false;
107 }
108
109 //change points
111 if ((y->x - x->x) / gvf_survey.dir_vec.x < 0.0) {
112 tmp = *x;
113 *x = *y;
114 *y = tmp;
115 }
116 } else if ((y->y - x->y) / gvf_survey.dir_vec.y < 0.0) {
117 tmp = *x;
118 *x = *y;
119 *y = tmp;
120 }
121
122 return true;
123}
124
135void gvf_nav_survey_polygon_setup(uint8_t first_wp, uint8_t size, float angle, float sweep_width, float shot_dist,
136 float min_rad, float altitude)
137{
138 int i;
139 struct FloatVect2 small, sweep;
140 float divider, angle_rad = angle / 180.0 * M_PI;
141
142 if (angle < 0.0) { angle += 360.0; }
143 if (angle >= 360.0) { angle -= 360.0; }
144
146 gvf_survey.poly_count = size;
147
148 gvf_survey.psa_sweep_width = sweep_width;
152
154 gvf_survey.return_angle = angle + 180;
155 if (gvf_survey.return_angle > 359) { gvf_survey.return_angle -= 360; }
156
157 if (angle <= 45.0 || angle >= 315.0) {
158 //north
159 gvf_survey.dir_vec.y = 1.0;
161 sweep.x = 1.0;
163 } else if (angle <= 135.0) {
164 //east
165 gvf_survey.dir_vec.x = 1.0;
167 sweep.y = -1.0;
169 } else if (angle <= 225.0) {
170 //south
171 gvf_survey.dir_vec.y = -1.0;
173 sweep.x = -1.0;
175 } else {
176 //west
177 gvf_survey.dir_vec.x = -1.0;
179 sweep.y = 1.0;
181 }
182
183 //normalize
185
188
189 //begin at leftmost position (relative to gvf_survey.dir_vec)
191
193
194 //calculate the leftmost point if one sees the dir vec as going "up" and the sweep vec as going right
195 if (divider < 0.0) {
196 for (i = 1; i < gvf_survey.poly_count; i++) {
198 (small.x - waypoints[gvf_survey.poly_first + i].x)) > 0.0) {
200 }
201 }
202 } else {
203 for (i = 1; i < gvf_survey.poly_count; i++) {
205 (small.x - waypoints[gvf_survey.poly_first + i].x)) > 0.0) {
207 }
208 }
209 }
210
211 //calculate the line the defines the first flyover
215
218 return;
219 }
220
221 //center of the entry circle
223
224 //fast climbing to desired altitude
227
229}
230
237{
238 if (rad > 0) {
240 } else {
242 }
243}
244
246{
249
250 //entry circle around entry-center until the desired altitude is reached
251 if (gvf_survey.stage == gENTRY) {
259#ifdef DIGITAL_CAM
262#endif
263 }
264 }
265 //fly the segment until seg_end is reached
266 if (gvf_survey.stage == gSEG) {
268 //calculate all needed points for the next flyover
270#ifdef DIGITAL_CAM
271 dc_stop();
272#endif
276
277 //if we get no intersection the survey is finished
278 static struct FloatVect2 sum_start_sweep;
279 static struct FloatVect2 sum_end_sweep;
283 return false;
284 }
285
288
291
294 }
295 }
296 //turn from stage to return
297 else if (gvf_survey.stage == gTURN1) {
303 }
304 //return
305 } else if (gvf_survey.stage == gRET) {
310 }
311 //turn from return to stage
312 } else if (gvf_survey.stage == gTURN2) {
319#ifdef DIGITAL_CAM
322#endif
323 }
324 }
325
326 return true;
327}
static int32_t altitude
Core autopilot interface common to all firmwares.
struct point waypoints[NB_WAYPOINT]
size == nb_waypoint, waypoint 0 is a dummy waypoint
Definition common_nav.c:44
float y
Definition common_nav.h:41
float x
Definition common_nav.h:40
uint8_t dc_survey(float interval, float x, float y)
Sets the dc control in distance mode.
Definition dc.c:240
uint8_t dc_stop(void)
Stop dc control.
Definition dc.c:262
Standard Digital Camera Control Interface.
#define FLOAT_VECT2_NORMALIZE(_v)
#define VECT2_SMUL(_vo, _vi, _s)
#define VECT2_DIFF(_c, _a, _b)
#define VECT2_COPY(_a, _b)
#define VECT2_SUM(_c, _a, _b)
static struct UtmCoor_f * stateGetPositionUtm_f(void)
Get position in UTM coordinates (float).
Definition state.h:821
bool gvf_segment_XY1_XY2(float x1, float y1, float x2, float y2)
Definition gvf.c:382
void gvf_set_direction(int8_t s)
Definition gvf.c:266
bool gvf_ellipse_XY(float x, float y, float a, float b, float alpha)
Definition gvf.c:433
Guidance algorithm based on vector fields.
static float p[2][2]
uint16_t foo
Definition main_demo5.c:58
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_init_stage(void)
needs to be implemented by fixedwing and rotorcraft seperately
Definition nav.c:92
float last_y
Definition nav.c:47
float last_x
Definition nav.c:47
Fixedwing Navigation library.
#define NavCourseCloseTo(x)
Definition nav.h:163
#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
static bool gvf_intercept_two_lines(struct FloatVect2 *p, struct FloatVect2 x, struct FloatVect2 y, float a1, float a2, float b1, float b2)
intercept two lines and give back the point of intersection
static bool gvf_get_two_intersects(struct FloatVect2 *x, struct FloatVect2 *y, struct FloatVect2 a, struct FloatVect2 b)
intersects a line with the polygon and gives back the two intersection points
void gvf_nav_direction_circle(float rad)
main navigation routine.
void gvf_nav_survey_polygon_setup(uint8_t first_wp, uint8_t size, float angle, float sweep_width, float shot_dist, float min_rad, float altitude)
initializes the variables needed for the survey to start
struct gvf_SurveyPolyAdv gvf_survey
bool gvf_nav_survey_polygon_run(void)
static void gvf_nav_points(struct FloatVect2 start, struct FloatVect2 end)
struct FloatVect2 seg_center2
struct FloatVect2 rad_vec
struct FloatVect2 ret_end
struct FloatVect2 entry_center
struct FloatVect2 seg_end
enum gvf_SurveyStage stage
struct FloatVect2 dir_vec
struct FloatVect2 seg_start
struct FloatVect2 sweep_vec
struct FloatVect2 seg_center1
struct FloatVect2 ret_start
#define CARROT
default approaching_time for a wp
Definition navigation.h:70
API to get/set the generic vehicle states.
unsigned char uint8_t
Typedef defining 8 bit unsigned char type.
float b
Definition wedgebug.c:202