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[fixedwing] convert disc_survey to module
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<!DOCTYPE module SYSTEM "module.dtd"> | ||
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<module name="nav_disc_survey" dir="nav"> | ||
<doc> | ||
<description> | ||
Disc Survey. | ||
</description> | ||
</doc> | ||
<header> | ||
<file name="nav_disc_survey.h"/> | ||
</header> | ||
<makefile> | ||
<file name="nav_disc_survey.c"/> | ||
</makefile> | ||
</module> |
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/* | ||
* Copyright (C) 2003-2005 Pascal Brisset, Antoine Drouin | ||
* | ||
* This file is part of paparazzi. | ||
* | ||
* paparazzi is free software; you can redistribute it and/or modify | ||
* it under the terms of the GNU General Public License as published by | ||
* the Free Software Foundation; either version 2, or (at your option) | ||
* any later version. | ||
* | ||
* paparazzi is distributed in the hope that it will be useful, | ||
* but WITHOUT ANY WARRANTY; without even the implied warranty of | ||
* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the | ||
* GNU General Public License for more details. | ||
* | ||
* You should have received a copy of the GNU General Public License | ||
* along with paparazzi; see the file COPYING. If not, write to | ||
* the Free Software Foundation, 59 Temple Place - Suite 330, | ||
* Boston, MA 02111-1307, USA. | ||
*/ | ||
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/** | ||
* @file modules/nav/nav_disc_survey.c | ||
* | ||
*/ | ||
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#include "modules/nav/nav_disc_survey.h" | ||
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#include "generated/airframe.h" | ||
#include "state.h" | ||
#include "std.h" | ||
#include "subsystems/nav.h" | ||
#include "generated/flight_plan.h" | ||
#include "math/pprz_algebra_float.h" | ||
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enum DiscSurveyStatus { UTURN, SEGMENT, DOWNWIND }; | ||
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struct DiscSurvey { | ||
enum DiscSurveyStatus status; | ||
int8_t sign; | ||
struct FloatVect2 c; | ||
struct FloatVect2 c1; | ||
struct FloatVect2 c2; | ||
}; | ||
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static struct DiscSurvey disc_survey; | ||
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bool_t nav_disc_survey_start( float grid ) { | ||
nav_survey_shift = grid; | ||
disc_survey.status = DOWNWIND; | ||
disc_survey.sign = 1; | ||
disc_survey.c1.x = stateGetPositionEnu_f()->x; | ||
disc_survey.c1.y = stateGetPositionEnu_f()->y; | ||
return FALSE; | ||
} | ||
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bool_t nav_disc_survey_run( uint8_t center_wp, float radius) { | ||
struct FloatVect2* wind = stateGetHorizontalWindspeed_f(); | ||
float wind_dir = atan2(wind->x, wind->y) + M_PI; | ||
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/** Not null even if wind_east=wind_north=0 */ | ||
struct FloatVect2 upwind; | ||
upwind.x = cos(wind_dir); | ||
upwind.y = sin(wind_dir); | ||
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float grid = nav_survey_shift / 2; | ||
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switch (disc_survey.status) { | ||
case UTURN: | ||
nav_circle_XY(disc_survey.c.x, disc_survey.c.y, grid*disc_survey.sign); | ||
if (NavQdrCloseTo(DegOfRad(M_PI_2-wind_dir))) { | ||
disc_survey.c1.x = stateGetPositionEnu_f()->x; | ||
disc_survey.c1.y = stateGetPositionEnu_f()->y; | ||
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struct FloatVect2 dist; | ||
VECT2_DIFF(dist, disc_survey.c1, waypoints[center_wp]); | ||
float d = FLOAT_VECT2_DOT_PRODUCT(upwind, dist); | ||
if (d > radius) { | ||
disc_survey.status = DOWNWIND; | ||
} else { | ||
float w = sqrtf(radius*radius - d*d) - 1.5*grid; | ||
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struct FloatVect2 crosswind; | ||
crosswind.x = -upwind.y; | ||
crosswind.y = upwind.x; | ||
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disc_survey.c2.x = waypoints[center_wp].x + d*upwind.x - w*disc_survey.sign*crosswind.x; | ||
disc_survey.c2.y = waypoints[center_wp].y + d*upwind.y - w*disc_survey.sign*crosswind.y; | ||
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disc_survey.status = SEGMENT; | ||
} | ||
nav_init_stage(); | ||
} | ||
break; | ||
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case DOWNWIND: | ||
disc_survey.c2.x = waypoints[center_wp].x - upwind.x * radius; | ||
disc_survey.c2.y = waypoints[center_wp].y - upwind.y * radius; | ||
disc_survey.status = SEGMENT; | ||
/* No break; */ | ||
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case SEGMENT: | ||
nav_route_xy(disc_survey.c1.x, disc_survey.c1.y, disc_survey.c2.x, disc_survey.c2.y); | ||
if (nav_approaching_xy(disc_survey.c2.x, disc_survey.c2.y, disc_survey.c1.x, disc_survey.c1.y, CARROT)) { | ||
disc_survey.c.x = disc_survey.c2.x + grid*upwind.x; | ||
disc_survey.c.y = disc_survey.c2.y + grid*upwind.y; | ||
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disc_survey.sign = -disc_survey.sign; | ||
disc_survey.status = UTURN; | ||
nav_init_stage(); | ||
} | ||
break; | ||
default: | ||
break; | ||
} | ||
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NavVerticalAutoThrottleMode(0.); /* No pitch */ | ||
NavVerticalAltitudeMode(WaypointAlt(center_wp), 0.); /* No preclimb */ | ||
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return TRUE; | ||
} |
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