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further progress on mixer node
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@ -182,6 +182,15 @@ target_link_libraries(att_estimator
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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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@ -1,4 +1,4 @@
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e/****************************************************************************
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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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@ -37,7 +37,19 @@ e/****************************************************************************
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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 <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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#define _rotor_count 4
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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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struct {
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float control[8];
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@ -47,16 +59,96 @@ e/****************************************************************************
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float control[8];
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}outputs;
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void mix(void *input) {
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const 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 Rotor *_rotors = { &_config_x[0]
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};
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void 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 actuatorControlsCallback(const PX4_TOPIC_T(actuator_controls_0) &msg)
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{
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// read message
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memcpy(inputs,msg,sizeof(inputs));
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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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@ -65,6 +157,7 @@ void mix(void *input) {
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ros::init(argc, argv, "mc_mixer");
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ros::NodeHandle n;
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ros::Subscriber sub = n.subscribe("actuator_controls_0", 1000, actuatorControlsCallback);
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ros::Publisher pub = n.advertise<mav_msgs::MotorSpeed>("mixed_motor_commands",10);
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ros::spin();
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