forked from Archive/PX4-Autopilot
Merge branch 'ros_dev_roman' into dev_ros
This commit is contained in:
commit
40f6e9f386
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@ -194,6 +194,15 @@ target_link_libraries(manual_input
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px4
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)
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## Multicopter Mixer dummy
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add_executable(mc_mixer
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src/platforms/ros/nodes/mc_mixer.cpp)
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add_dependencies(mc_mixer px4_generate_messages_cpp)
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target_link_libraries(mc_mixer
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${catkin_LIBRARIES}
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px4
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)
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#############
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## Install ##
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@ -0,0 +1,184 @@
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/****************************************************************************
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*
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* Copyright (c) 2014 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 att_estimator.cpp
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* Dummy attitude estimator that forwards attitude from gazebo to px4 topic
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*
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* @author Roman Bapst <romanbapst@yahoo.de>
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*/
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#include <ros/ros.h>
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#include <px4.h>
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#include <lib/mathlib/mathlib.h>
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#include <mav_msgs/MotorSpeed.h>
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class MultirotorMixer {
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public:
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MultirotorMixer();
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struct Rotor {
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float roll_scale;
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float pitch_scale;
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float yaw_scale;
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};
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void actuatorControlsCallback(const PX4_TOPIC_T(actuator_controls_0) &msg);
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private:
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ros::NodeHandle _n;
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ros::Subscriber _sub;
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ros::Publisher _pub;
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const Rotor *_rotors;
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unsigned _rotor_count;
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struct {
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float control[6];
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}inputs;
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struct {
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float control[6];
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}outputs;
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void mix();
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};
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const MultirotorMixer::Rotor _config_x[] = {
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{ 0.000000, -1.000000, -1.00 },
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{ -0.000000, 1.000000, -1.00 },
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{ 1.000000, 0.000000, 1.00 },
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{ -1.000000, 0.000000, 1.00 },
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};
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const MultirotorMixer::Rotor *_config_index = { &_config_x[0]
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};
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MultirotorMixer::MultirotorMixer():
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_rotor_count(4),
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_rotors(_config_index)
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{
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_sub = _n.subscribe("actuator_controls_0", 1000, &MultirotorMixer::actuatorControlsCallback,this);
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_pub = _n.advertise<mav_msgs::MotorSpeed>("mixed_motor_commands",10);
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}
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void MultirotorMixer::mix() {
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float roll = math::constrain(inputs.control[0], -1.0f, 1.0f);
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float pitch = math::constrain(inputs.control[1], -1.0f, 1.0f);
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float yaw = math::constrain(inputs.control[2], -1.0f, 1.0f);
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float thrust = math::constrain(inputs.control[3], 0.0f, 1.0f);
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float min_out = 0.0f;
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float max_out = 0.0f;
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/* perform initial mix pass yielding unbounded outputs, ignore yaw */
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for (unsigned i = 0; i < _rotor_count; i++) {
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float out = roll * _rotors[i].roll_scale
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+ pitch * _rotors[i].pitch_scale + thrust;
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/* limit yaw if it causes outputs clipping */
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if (out >= 0.0f && out < -yaw * _rotors[i].yaw_scale) {
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yaw = -out / _rotors[i].yaw_scale;
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}
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/* calculate min and max output values */
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if (out < min_out) {
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min_out = out;
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}
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if (out > max_out) {
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max_out = out;
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}
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outputs.control[i] = out;
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}
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/* scale down roll/pitch controls if some outputs are negative, don't add yaw, keep total thrust */
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if (min_out < 0.0f) {
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float scale_in = thrust / (thrust - min_out);
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/* mix again with adjusted controls */
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for (unsigned i = 0; i < _rotor_count; i++) {
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outputs.control[i] = scale_in
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* (roll * _rotors[i].roll_scale
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+ pitch * _rotors[i].pitch_scale) + thrust;
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}
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} else {
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/* roll/pitch mixed without limiting, add yaw control */
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for (unsigned i = 0; i < _rotor_count; i++) {
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outputs.control[i] += yaw * _rotors[i].yaw_scale;
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}
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}
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/* scale down all outputs if some outputs are too large, reduce total thrust */
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float scale_out;
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if (max_out > 1.0f) {
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scale_out = 1.0f / max_out;
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} else {
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scale_out = 1.0f;
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}
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/* scale outputs to range _idle_speed..1, and do final limiting */
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for (unsigned i = 0; i < _rotor_count; i++) {
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outputs.control[i] = math::constrain(outputs.control[i], 0.0f, 1.0f);
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}
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}
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void MultirotorMixer::actuatorControlsCallback(const PX4_TOPIC_T(actuator_controls_0) &msg)
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{
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// read message
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for(int i = 0;i < msg.NUM_ACTUATOR_CONTROLS;i++) {
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inputs.control[i] = msg.control[i];
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}
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// mix
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mix();
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// publish message
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mav_msgs::MotorSpeed rotor_vel_msg;
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for (int i = 0; i < _rotor_count; i++) {
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rotor_vel_msg.motor_speed.push_back(outputs.control[i]);
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}
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_pub.publish(rotor_vel_msg);
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}
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int main(int argc, char **argv)
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{
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ros::init(argc, argv, "mc_mixer");
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MultirotorMixer mixer;
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ros::spin();
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return 0;
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}
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