mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-31 02:31:36 +08:00
Halfway-working fixed wing waypoint control, needs more effort
This commit is contained in:
File diff suppressed because it is too large
Load Diff
@@ -1,7 +1,7 @@
|
|||||||
/****************************************************************************
|
/****************************************************************************
|
||||||
*
|
*
|
||||||
* Copyright (C) 2008-2012 PX4 Development Team. All rights reserved.
|
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
|
||||||
* Author: @author Lorenz Meier <lm@inf.ethz.ch>
|
* Author: Lorenz Meier <lm@inf.ethz.ch>
|
||||||
*
|
*
|
||||||
* Redistribution and use in source and binary forms, with or without
|
* Redistribution and use in source and binary forms, with or without
|
||||||
* modification, are permitted provided that the following conditions
|
* modification, are permitted provided that the following conditions
|
||||||
@@ -36,6 +36,8 @@
|
|||||||
* @file multirotor_att_control_main.c
|
* @file multirotor_att_control_main.c
|
||||||
*
|
*
|
||||||
* Implementation of multirotor attitude control main loop.
|
* Implementation of multirotor attitude control main loop.
|
||||||
|
*
|
||||||
|
* @author Lorenz Meier <lm@inf.ethz.ch>
|
||||||
*/
|
*/
|
||||||
|
|
||||||
#include <nuttx/config.h>
|
#include <nuttx/config.h>
|
||||||
|
|||||||
@@ -51,46 +51,6 @@
|
|||||||
|
|
||||||
#include "multirotor_position_control.h"
|
#include "multirotor_position_control.h"
|
||||||
|
|
||||||
float get_distance_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next)
|
|
||||||
{
|
|
||||||
double lat_now_rad = lat_now / 180.0 * M_PI;
|
|
||||||
double lon_now_rad = lon_now / 180.0 * M_PI;
|
|
||||||
double lat_next_rad = lat_next / 180.0 * M_PI;
|
|
||||||
double lon_next_rad = lon_next / 180.0 * M_PI;
|
|
||||||
|
|
||||||
|
|
||||||
double d_lat = lat_next_rad - lat_now_rad;
|
|
||||||
double d_lon = lon_next_rad - lon_now_rad;
|
|
||||||
|
|
||||||
double a = sin(d_lat / 2.0) * sin(d_lat / 2.0) + sin(d_lon / 2.0) * sin(d_lon / 2.0) * cos(lat_now_rad) * cos(lat_next_rad);
|
|
||||||
double c = 2 * atan2(sqrt(a), sqrt(1 - a));
|
|
||||||
|
|
||||||
const double radius_earth = 6371000.0;
|
|
||||||
|
|
||||||
return radius_earth * c;
|
|
||||||
}
|
|
||||||
|
|
||||||
float get_bearing_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next)
|
|
||||||
{
|
|
||||||
double lat_now_rad = lat_now / 180.0 * M_PI;
|
|
||||||
double lon_now_rad = lon_now / 180.0 * M_PI;
|
|
||||||
double lat_next_rad = lat_next / 180.0 * M_PI;
|
|
||||||
double lon_next_rad = lon_next / 180.0 * M_PI;
|
|
||||||
|
|
||||||
double d_lat = lat_next_rad - lat_now_rad;
|
|
||||||
double d_lon = lon_next_rad - lon_now_rad;
|
|
||||||
|
|
||||||
/* conscious mix of double and float trig function to maximize speed and efficiency */
|
|
||||||
float theta = atan2f(sin(d_lon) * cos(lat_next_rad) , cos(lat_now_rad) * sin(lat_next_rad) - sin(lat_now_rad) * cos(lat_next_rad) * cos(d_lon));
|
|
||||||
|
|
||||||
// XXX wrapping check is incomplete
|
|
||||||
if (theta < 0.0f) {
|
|
||||||
theta = theta + 2.0f * M_PI_F;
|
|
||||||
}
|
|
||||||
|
|
||||||
return theta;
|
|
||||||
}
|
|
||||||
|
|
||||||
void control_multirotor_position(const struct vehicle_state_s *vstatus, const struct vehicle_manual_control_s *manual,
|
void control_multirotor_position(const struct vehicle_state_s *vstatus, const struct vehicle_manual_control_s *manual,
|
||||||
const struct vehicle_attitude_s *att, const struct vehicle_local_position_s *local_pos,
|
const struct vehicle_attitude_s *att, const struct vehicle_local_position_s *local_pos,
|
||||||
const struct vehicle_local_position_setpoint_s *local_pos_sp, struct vehicle_attitude_setpoint_s *att_sp)
|
const struct vehicle_local_position_setpoint_s *local_pos_sp, struct vehicle_attitude_setpoint_s *att_sp)
|
||||||
|
|||||||
@@ -48,7 +48,8 @@ CSRCS = err.c \
|
|||||||
#
|
#
|
||||||
ifeq ($(TARGET),px4fmu)
|
ifeq ($(TARGET),px4fmu)
|
||||||
CSRCS += systemlib.c \
|
CSRCS += systemlib.c \
|
||||||
pid/pid.c
|
pid/pid.c \
|
||||||
|
geo/geo.c
|
||||||
endif
|
endif
|
||||||
|
|
||||||
include $(APPDIR)/mk/app.mk
|
include $(APPDIR)/mk/app.mk
|
||||||
|
|||||||
@@ -0,0 +1,88 @@
|
|||||||
|
/****************************************************************************
|
||||||
|
*
|
||||||
|
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
|
||||||
|
* Author: Thomas Gubler <thomasgubler@student.ethz.ch>
|
||||||
|
* Julian Oes <joes@student.ethz.ch>
|
||||||
|
* Lorenz Meier <lm@inf.ethz.ch>
|
||||||
|
*
|
||||||
|
* Redistribution and use in source and binary forms, with or without
|
||||||
|
* modification, are permitted provided that the following conditions
|
||||||
|
* are met:
|
||||||
|
*
|
||||||
|
* 1. Redistributions of source code must retain the above copyright
|
||||||
|
* notice, this list of conditions and the following disclaimer.
|
||||||
|
* 2. Redistributions in binary form must reproduce the above copyright
|
||||||
|
* notice, this list of conditions and the following disclaimer in
|
||||||
|
* the documentation and/or other materials provided with the
|
||||||
|
* distribution.
|
||||||
|
* 3. Neither the name PX4 nor the names of its contributors may be
|
||||||
|
* used to endorse or promote products derived from this software
|
||||||
|
* without specific prior written permission.
|
||||||
|
*
|
||||||
|
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
|
||||||
|
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
|
||||||
|
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
|
||||||
|
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
|
||||||
|
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
|
||||||
|
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
|
||||||
|
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
|
||||||
|
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
|
||||||
|
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
|
||||||
|
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
|
||||||
|
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
|
||||||
|
* POSSIBILITY OF SUCH DAMAGE.
|
||||||
|
*
|
||||||
|
****************************************************************************/
|
||||||
|
|
||||||
|
/**
|
||||||
|
* @file geo.c
|
||||||
|
*
|
||||||
|
* Geo / math functions to perform geodesic calculations
|
||||||
|
*
|
||||||
|
* @author Thomas Gubler <thomasgubler@student.ethz.ch>
|
||||||
|
* @author Julian Oes <joes@student.ethz.ch>
|
||||||
|
* @author Lorenz Meier <lm@inf.ethz.ch>
|
||||||
|
*/
|
||||||
|
|
||||||
|
#include <systemlib/geo/geo.h>
|
||||||
|
#include <math.h>
|
||||||
|
|
||||||
|
__EXPORT float get_distance_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next)
|
||||||
|
{
|
||||||
|
double lat_now_rad = lat_now / 180.0 * M_PI;
|
||||||
|
double lon_now_rad = lon_now / 180.0 * M_PI;
|
||||||
|
double lat_next_rad = lat_next / 180.0 * M_PI;
|
||||||
|
double lon_next_rad = lon_next / 180.0 * M_PI;
|
||||||
|
|
||||||
|
|
||||||
|
double d_lat = lat_next_rad - lat_now_rad;
|
||||||
|
double d_lon = lon_next_rad - lon_now_rad;
|
||||||
|
|
||||||
|
double a = sin(d_lat / 2.0) * sin(d_lat / 2.0) + sin(d_lon / 2.0) * sin(d_lon / 2.0) * cos(lat_now_rad) * cos(lat_next_rad);
|
||||||
|
double c = 2 * atan2(sqrt(a), sqrt(1 - a));
|
||||||
|
|
||||||
|
const double radius_earth = 6371000.0;
|
||||||
|
|
||||||
|
return radius_earth * c;
|
||||||
|
}
|
||||||
|
|
||||||
|
__EXPORT float get_bearing_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next)
|
||||||
|
{
|
||||||
|
double lat_now_rad = lat_now / 180.0 * M_PI;
|
||||||
|
double lon_now_rad = lon_now / 180.0 * M_PI;
|
||||||
|
double lat_next_rad = lat_next / 180.0 * M_PI;
|
||||||
|
double lon_next_rad = lon_next / 180.0 * M_PI;
|
||||||
|
|
||||||
|
double d_lat = lat_next_rad - lat_now_rad;
|
||||||
|
double d_lon = lon_next_rad - lon_now_rad;
|
||||||
|
|
||||||
|
/* conscious mix of double and float trig function to maximize speed and efficiency */
|
||||||
|
float theta = atan2f(sin(d_lon) * cos(lat_next_rad) , cos(lat_now_rad) * sin(lat_next_rad) - sin(lat_now_rad) * cos(lat_next_rad) * cos(d_lon));
|
||||||
|
|
||||||
|
// XXX wrapping check is incomplete
|
||||||
|
if (theta < 0.0f) {
|
||||||
|
theta = theta + 2.0f * M_PI_F;
|
||||||
|
}
|
||||||
|
|
||||||
|
return theta;
|
||||||
|
}
|
||||||
@@ -0,0 +1,49 @@
|
|||||||
|
/****************************************************************************
|
||||||
|
*
|
||||||
|
* Copyright (C) 2012 PX4 Development Team. All rights reserved.
|
||||||
|
* Author: Thomas Gubler <thomasgubler@student.ethz.ch>
|
||||||
|
* Julian Oes <joes@student.ethz.ch>
|
||||||
|
* Lorenz Meier <lm@inf.ethz.ch>
|
||||||
|
*
|
||||||
|
* Redistribution and use in source and binary forms, with or without
|
||||||
|
* modification, are permitted provided that the following conditions
|
||||||
|
* are met:
|
||||||
|
*
|
||||||
|
* 1. Redistributions of source code must retain the above copyright
|
||||||
|
* notice, this list of conditions and the following disclaimer.
|
||||||
|
* 2. Redistributions in binary form must reproduce the above copyright
|
||||||
|
* notice, this list of conditions and the following disclaimer in
|
||||||
|
* the documentation and/or other materials provided with the
|
||||||
|
* distribution.
|
||||||
|
* 3. Neither the name PX4 nor the names of its contributors may be
|
||||||
|
* used to endorse or promote products derived from this software
|
||||||
|
* without specific prior written permission.
|
||||||
|
*
|
||||||
|
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
|
||||||
|
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
|
||||||
|
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
|
||||||
|
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
|
||||||
|
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
|
||||||
|
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
|
||||||
|
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
|
||||||
|
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
|
||||||
|
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
|
||||||
|
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
|
||||||
|
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
|
||||||
|
* POSSIBILITY OF SUCH DAMAGE.
|
||||||
|
*
|
||||||
|
****************************************************************************/
|
||||||
|
|
||||||
|
/**
|
||||||
|
* @file geo.h
|
||||||
|
*
|
||||||
|
* Definition of geo / math functions to perform geodesic calculations
|
||||||
|
*
|
||||||
|
* @author Thomas Gubler <thomasgubler@student.ethz.ch>
|
||||||
|
* @author Julian Oes <joes@student.ethz.ch>
|
||||||
|
* @author Lorenz Meier <lm@inf.ethz.ch>
|
||||||
|
*/
|
||||||
|
|
||||||
|
__EXPORT float get_distance_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next);
|
||||||
|
|
||||||
|
__EXPORT float get_bearing_to_next_waypoint(double lat_now, double lon_now, double lat_next, double lon_next);
|
||||||
Reference in New Issue
Block a user