/**************************************************************************** * * Copyright (c) 2016 PX4 Development Team. All rights reserved. * * 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 output.cpp * @author Leon Müller (thedevleon) * @author Beat Küng * */ #include "output.h" #include #include #include #include #include #include #define LATLON_TO_M 0.01113195 namespace vmount { OutputBase::OutputBase(const OutputConfig &output_config) : _config(output_config) { _last_update = hrt_absolute_time(); } OutputBase::~OutputBase() { if (_vehicle_attitude_sub >= 0) { orb_unsubscribe(_vehicle_attitude_sub); } if (_vehicle_global_position_sub >= 0) { orb_unsubscribe(_vehicle_global_position_sub); } } int OutputBase::initialize() { if ((_vehicle_attitude_sub = orb_subscribe(ORB_ID(vehicle_attitude))) < 0) { return -errno; } if ((_vehicle_global_position_sub = orb_subscribe(ORB_ID(vehicle_global_position))) < 0) { return -errno; } return 0; } float OutputBase::_calculate_pitch(double lon, double lat, float altitude, const vehicle_global_position_s &global_position) { double scale = cos(M_DEG_TO_RAD * ((global_position.lat + lat) * 0.00000005)); float x = (float)((lon - global_position.lon) * scale * LATLON_TO_M); float y = (float)((lat - global_position.lat) * LATLON_TO_M); float z = altitude - global_position.alt; float target_distance = sqrtf(x * x + y * y); return atan2f(z, target_distance) * (float)M_RAD_TO_DEG; } void OutputBase::_set_angle_setpoints(const ControlData *control_data) { _cur_control_data = control_data; for (int i = 0; i < 3; ++i) { _stabilize[i] = control_data->stabilize_axis[i]; _angle_speeds[i] = 0.f; } switch (control_data->type) { case ControlData::Type::Angle: for (int i = 0; i < 3; ++i) { if (control_data->type_data.angle.is_speed[i]) { _angle_speeds[i] = control_data->type_data.angle.angles[i]; } else { _angle_setpoints[i] = control_data->type_data.angle.angles[i]; } } break; case ControlData::Type::LonLat: _handle_position_update(true); break; case ControlData::Type::Neutral: _angle_setpoints[0] = 0.f; _angle_setpoints[1] = 0.f; _angle_setpoints[2] = 0.f; break; } } void OutputBase::_handle_position_update(bool force_update) { bool need_update = force_update; if (!_cur_control_data || _cur_control_data->type != ControlData::Type::LonLat) { return; } if (!force_update) { orb_check(_vehicle_global_position_sub, &need_update); } if (!need_update) { return; } vehicle_global_position_s vehicle_global_position; orb_copy(ORB_ID(vehicle_global_position), _vehicle_global_position_sub, &vehicle_global_position); float pitch; const double &lon = _cur_control_data->type_data.lonlat.lon; const double &lat = _cur_control_data->type_data.lonlat.lat; const float &alt = _cur_control_data->type_data.lonlat.altitude; if (_cur_control_data->type_data.lonlat.pitch_fixed_angle >= -M_PI_F) { pitch = _cur_control_data->type_data.lonlat.pitch_fixed_angle; } else { pitch = _calculate_pitch(lon, lat, alt, vehicle_global_position); } float roll = _cur_control_data->type_data.lonlat.roll_angle; float yaw = get_bearing_to_next_waypoint(vehicle_global_position.lat, vehicle_global_position.lon, lat, lon) * (float)M_RAD_TO_DEG; _angle_setpoints[0] = roll; _angle_setpoints[1] = pitch; _angle_setpoints[2] = yaw; } void OutputBase::_calculate_output_angles(const hrt_abstime &t) { //take speed into account float dt = (t - _last_update) / 1.e6f; for (int i = 0; i < 3; ++i) { _angle_setpoints[i] += dt * _angle_speeds[i]; } //get the output angles and stabilize if necessary vehicle_attitude_s vehicle_attitude; if (_stabilize[0] || _stabilize[1] || _stabilize[2]) { orb_copy(ORB_ID(vehicle_attitude), _vehicle_attitude_sub, &vehicle_attitude); } float att[3] = { vehicle_attitude.roll, vehicle_attitude.pitch, vehicle_attitude.yaw }; for (int i = 0; i < 3; ++i) { if (_stabilize[i]) { _angle_outputs[i] = _angle_setpoints[i] - att[i]; } else { _angle_outputs[i] = _angle_setpoints[i]; } //bring angles into proper range [-pi, pi] while (_angle_outputs[i] > M_PI_F) { _angle_outputs[i] -= 2.f * M_PI_F; } while (_angle_outputs[i] < -M_PI_F) { _angle_outputs[i] += 2.f * M_PI_F; } } } } /* namespace vmount */