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nav.h
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nav.h
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/*
* Copyright (C) 2003-2009 ENAC, 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.
*/
/**
* @file firmwares/fixedwing/nav.h
*
* Fixedwing Navigation library.
*
* This collection of macros and functions is used by the C code generated
* from the XML flight plan.
*/
#ifndef NAV_H
#define NAV_H
#include "std.h"
#include "paparazzi.h"
#include "state.h"
#ifdef CTRL_TYPE_H
#include CTRL_TYPE_H
#endif
#include "subsystems/navigation/nav_survey_rectangle.h"
#include "subsystems/navigation/common_flight_plan.h"
#include "subsystems/navigation/common_nav.h"
#define NAV_GRAVITY 9.806
#define Square(_x) ((_x)*(_x))
#define DistanceSquare(p1_x, p1_y, p2_x, p2_y) (Square(p1_x-p2_x)+Square(p1_y-p2_y))
enum oval_status { OR12, OC2, OR21, OC1 };
extern float cur_pos_x;
extern float cur_pos_y;
extern float last_x, last_y;
extern float desired_x, desired_y, nav_altitude, flight_altitude, nav_glide_pitch_trim;
extern pprz_t nav_throttle_setpoint;
extern float nav_pitch; /* Rad */
extern float rc_pitch;
extern float fp_pitch; /* Degrees */
extern float carrot_x, carrot_y;
extern float nav_circle_radians; /* Cumulated */
extern float nav_circle_radians_no_rewind; /* Cumulated */
extern bool_t nav_in_circle;
extern bool_t nav_in_segment;
extern float nav_circle_x, nav_circle_y, nav_circle_radius; /* m */
extern float nav_segment_x_1, nav_segment_y_1, nav_segment_x_2, nav_segment_y_2; /* m */
extern int nav_mode;
#define NAV_MODE_ROLL 1
#define NAV_MODE_COURSE 2
extern uint8_t horizontal_mode;
#define HORIZONTAL_MODE_WAYPOINT 0
#define HORIZONTAL_MODE_ROUTE 1
#define HORIZONTAL_MODE_CIRCLE 2
extern void fly_to_xy(float x, float y);
#define NavGotoWaypoint(_wp) { \
horizontal_mode = HORIZONTAL_MODE_WAYPOINT; \
fly_to_xy(waypoints[_wp].x, waypoints[_wp].y); \
}
extern void nav_eight_init( void );
extern void nav_eight(uint8_t, uint8_t, float);
#define Eight(a, b, c) nav_eight((a), (b), (c))
extern void nav_oval_init( void );
extern void nav_oval(uint8_t, uint8_t, float);
extern uint8_t nav_oval_count;
#define Oval(a, b, c) nav_oval((b), (a), (c))
extern float nav_radius; /* m */
extern float nav_course; /* degrees, clockwise, 0.0 = N */
extern float nav_climb; /* m/s */
extern float nav_shift; /* Lateral shift along a route. In meters */
extern float nav_ground_speed_pgain, nav_ground_speed_setpoint;
extern float nav_survey_shift;
extern float nav_survey_west, nav_survey_east, nav_survey_north, nav_survey_south;
extern bool_t nav_survey_active;
void nav_periodic_task(void);
void nav_home(void);
void nav_init(void);
void nav_without_gps(void);
extern float nav_circle_trigo_qdr; /** Angle from center to mobile */
extern void nav_circle_XY(float x, float y, float radius);
#define NavCircleWaypoint(wp, radius) \
nav_circle_XY(waypoints[wp].x, waypoints[wp].y, radius)
/** Normalize a degree angle between 0 and 359 */
#define NormCourse(x) { \
uint8_t dont_loop_forever = 0; \
while (x < 0 && ++dont_loop_forever) x += 360; \
while (x >= 360 && ++dont_loop_forever) x -= 360; \
}
#define NavCircleCountNoRewind() (nav_circle_radians_no_rewind / (2*M_PI))
#define NavCircleCount() (fabs(nav_circle_radians) / (2*M_PI))
#define NavCircleQdr() ({ float qdr = DegOfRad(M_PI_2 - nav_circle_trigo_qdr); NormCourse(qdr); qdr; })
#define CloseDegAngles(_c1, _c2) ({ float _diff = _c1 - _c2; NormCourse(_diff); 350 < _diff || _diff < 10; })
/** True if x (in degrees) is close to the current QDR (less than 10 degrees)*/
#define NavQdrCloseTo(x) CloseDegAngles(x, NavCircleQdr())
#define NavCourseCloseTo(x) CloseDegAngles(x, DegOfRad(*stateGetHorizontalSpeedDir_f()))
/*********** Navigation along a line *************************************/
extern void nav_route_xy(float last_wp_x, float last_wp_y, float wp_x, float wp_y);
#define NavSegment(_start, _end) \
nav_route_xy(waypoints[_start].x, waypoints[_start].y, waypoints[_end].x, waypoints[_end].y)
bool_t nav_approaching_xy(float x, float y, float from_x, float from_y, float approaching_time);
#define NavApproaching(wp, time) nav_approaching_xy(waypoints[wp].x, waypoints[wp].y, last_x, last_y, time)
#define NavApproachingFrom(wp, from, time) nav_approaching_xy(waypoints[wp].x, waypoints[wp].y, waypoints[from].x, waypoints[from].y, time)
/** Set the climb control to auto-throttle with the specified pitch
pre-command */
#define NavVerticalAutoThrottleMode(_pitch) { \
v_ctl_climb_mode = V_CTL_CLIMB_MODE_AUTO_THROTTLE; \
nav_pitch = _pitch; \
}
/** Set the climb control to auto-pitch with the specified throttle
pre-command */
#define NavVerticalAutoPitchMode(_throttle) { \
v_ctl_climb_mode = V_CTL_CLIMB_MODE_AUTO_PITCH; \
nav_throttle_setpoint = _throttle; \
}
/** Set the vertical mode to altitude control with the specified altitude
setpoint and climb pre-command. */
#define NavVerticalAltitudeMode(_alt, _pre_climb) { \
v_ctl_mode = V_CTL_MODE_AUTO_ALT; \
nav_altitude = _alt; \
v_ctl_altitude_pre_climb = _pre_climb; \
}
/** Set the vertical mode to climb control with the specified climb setpoint */
#define NavVerticalClimbMode(_climb) { \
v_ctl_mode = V_CTL_MODE_AUTO_CLIMB; \
v_ctl_climb_setpoint = _climb; \
}
/** Set the vertical mode to fixed throttle with the specified setpoint */
#define NavVerticalThrottleMode(_throttle) { \
v_ctl_mode = V_CTL_MODE_AUTO_THROTTLE; \
nav_throttle_setpoint = _throttle; \
}
#define NavHeading(_course) { \
lateral_mode = LATERAL_MODE_COURSE; \
h_ctl_course_setpoint = _course; \
}
#define NavAttitude(_roll) { \
lateral_mode = LATERAL_MODE_ROLL; \
if(pprz_mode != PPRZ_MODE_AUTO1) \
{h_ctl_roll_setpoint = _roll;} \
}
#define nav_IncreaseShift(x) { if (x==0) nav_shift = 0; else nav_shift += x; }
#define nav_SetNavRadius(x) { if (x==1) nav_radius = DEFAULT_CIRCLE_RADIUS; else if (x==-1) nav_radius = -DEFAULT_CIRCLE_RADIUS; else nav_radius = x; }
#define NavKillThrottle() { kill_throttle = 1; }
#define GetPosX() (stateGetPositionEnu_f()->x)
#define GetPosY() (stateGetPositionEnu_f()->y)
#define GetPosAlt() (stateGetPositionUtm_f()->alt)
#define GetAltRef() (ground_alt)
#define SEND_NAVIGATION(_trans, _dev) { \
uint8_t _circle_count = NavCircleCount(); \
struct EnuCoor_f* pos = stateGetPositionEnu_f(); \
float dist_wp = sqrtf(dist2_to_wp); \
float dist_home = sqrtf(dist2_to_home); \
DOWNLINK_SEND_NAVIGATION(_trans, _dev, &nav_block, &nav_stage, &(pos->x), &(pos->y), &dist_wp, &dist_home, &_circle_count, &nav_oval_count); \
}
extern bool_t DownlinkSendWpNr(int _wp);
#define DownlinkSendWp(_trans, _dev, i) { \
float x = nav_utm_east0 + waypoints[i].x; \
float y = nav_utm_north0 + waypoints[i].y; \
DOWNLINK_SEND_WP_MOVED(_trans, _dev, &i, &x, &y, &(waypoints[i].a),&nav_utm_zone0); \
}
#endif /* NAV_H */