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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 mc_mixer.cpp |
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* Dummy multicopter mixer for euroc simulator (gazebo) |
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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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