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This splits vmount into inputs and outputs modules with a small API in between. It allows for greater flexibility, as any input method can be combined with any output method. At the same time it is easy to add a new input or output module.
206 lines
5.9 KiB
C++
206 lines
5.9 KiB
C++
/****************************************************************************
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*
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* Copyright (c) 2016 PX4 Development Team. All rights reserved.
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file output.cpp
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* @author Leon Müller (thedevleon)
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* @author Beat Küng <beat-kueng@gmx.net>
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*
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*/
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#include "output.h"
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#include <errno.h>
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#include <uORB/topics/vehicle_attitude.h>
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#include <uORB/topics/vehicle_global_position.h>
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#include <px4_defines.h>
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#include <geo/geo.h>
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#include <math.h>
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#define LATLON_TO_M 0.01113195
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namespace vmount
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{
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OutputBase::OutputBase(const OutputConfig &output_config)
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: _config(output_config)
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{
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_last_update = hrt_absolute_time();
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}
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OutputBase::~OutputBase()
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{
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if (_vehicle_attitude_sub >= 0) {
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orb_unsubscribe(_vehicle_attitude_sub);
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}
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if (_vehicle_global_position_sub >= 0) {
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orb_unsubscribe(_vehicle_global_position_sub);
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}
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}
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int OutputBase::initialize()
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{
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if ((_vehicle_attitude_sub = orb_subscribe(ORB_ID(vehicle_attitude))) < 0) {
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return -errno;
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}
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if ((_vehicle_global_position_sub = orb_subscribe(ORB_ID(vehicle_global_position))) < 0) {
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return -errno;
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}
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return 0;
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}
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float OutputBase::_calculate_pitch(double lon, double lat, float altitude,
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const vehicle_global_position_s &global_position)
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{
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double scale = cos(M_DEG_TO_RAD * ((global_position.lat + lat) * 0.00000005));
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float x = (float)((lon - global_position.lon) * scale * LATLON_TO_M);
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float y = (float)((lat - global_position.lat) * LATLON_TO_M);
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float z = altitude - global_position.alt;
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float target_distance = sqrtf(x * x + y * y);
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return atan2f(z, target_distance) * (float)M_RAD_TO_DEG;
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}
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void OutputBase::_set_angle_setpoints(const ControlData *control_data)
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{
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_cur_control_data = control_data;
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for (int i = 0; i < 3; ++i) {
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_stabilize[i] = control_data->stabilize_axis[i];
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_angle_speeds[i] = 0.f;
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}
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switch (control_data->type) {
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case ControlData::Type::Angle:
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for (int i = 0; i < 3; ++i) {
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if (control_data->type_data.angle.is_speed[i]) {
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_angle_speeds[i] = control_data->type_data.angle.angles[i];
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} else {
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_angle_setpoints[i] = control_data->type_data.angle.angles[i];
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}
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}
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break;
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case ControlData::Type::LonLat:
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_handle_position_update(true);
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break;
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case ControlData::Type::Neutral:
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_angle_setpoints[0] = 0.f;
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_angle_setpoints[1] = 0.f;
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_angle_setpoints[2] = 0.f;
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break;
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}
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}
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void OutputBase::_handle_position_update(bool force_update)
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{
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bool need_update = force_update;
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if (!_cur_control_data || _cur_control_data->type != ControlData::Type::LonLat) {
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return;
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}
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if (!force_update) {
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orb_check(_vehicle_global_position_sub, &need_update);
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}
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if (!need_update) {
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return;
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}
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vehicle_global_position_s vehicle_global_position;
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orb_copy(ORB_ID(vehicle_global_position), _vehicle_global_position_sub, &vehicle_global_position);
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float pitch;
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const double &lon = _cur_control_data->type_data.lonlat.lon;
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const double &lat = _cur_control_data->type_data.lonlat.lat;
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const float &alt = _cur_control_data->type_data.lonlat.altitude;
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if (_cur_control_data->type_data.lonlat.pitch_fixed_angle >= -M_PI_F) {
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pitch = _cur_control_data->type_data.lonlat.pitch_fixed_angle;
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} else {
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pitch = _calculate_pitch(lon, lat, alt, vehicle_global_position);
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}
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float roll = _cur_control_data->type_data.lonlat.roll_angle;
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float yaw = get_bearing_to_next_waypoint(vehicle_global_position.lat, vehicle_global_position.lon,
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lat, lon) * (float)M_RAD_TO_DEG;
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_angle_setpoints[0] = roll;
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_angle_setpoints[1] = pitch;
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_angle_setpoints[2] = yaw;
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}
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void OutputBase::_calculate_output_angles(const hrt_abstime &t)
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{
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//take speed into account
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float dt = (t - _last_update) / 1.e6f;
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for (int i = 0; i < 3; ++i) {
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_angle_setpoints[i] += dt * _angle_speeds[i];
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}
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//get the output angles and stabilize if necessary
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vehicle_attitude_s vehicle_attitude;
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if (_stabilize[0] || _stabilize[1] || _stabilize[2]) {
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orb_copy(ORB_ID(vehicle_attitude), _vehicle_attitude_sub, &vehicle_attitude);
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}
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float att[3] = { vehicle_attitude.roll, vehicle_attitude.pitch, vehicle_attitude.yaw };
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for (int i = 0; i < 3; ++i) {
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if (_stabilize[i]) {
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_angle_outputs[i] = _angle_setpoints[i] - att[i];
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} else {
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_angle_outputs[i] = _angle_setpoints[i];
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}
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//bring angles into proper range [-pi, pi]
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while (_angle_outputs[i] > M_PI_F) { _angle_outputs[i] -= 2.f * M_PI_F; }
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while (_angle_outputs[i] < -M_PI_F) { _angle_outputs[i] += 2.f * M_PI_F; }
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}
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}
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} /* namespace vmount */
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