further progress on mixer node

This commit is contained in:
Roman Bapst 2014-12-30 11:06:40 +01:00
parent 67c4930315
commit 484020177d
2 changed files with 106 additions and 4 deletions

View File

@ -182,6 +182,15 @@ target_link_libraries(att_estimator
px4
)
## Multicopter Mixer dummy
add_executable(mc_mixer
src/platforms/ros/nodes/mc_mixer.cpp)
add_dependencies(mc_mixer px4_generate_messages_cpp)
target_link_libraries(mc_mixer
${catkin_LIBRARIES}
px4
)
#############
## Install ##

View File

@ -1,4 +1,4 @@
e/****************************************************************************
/****************************************************************************
*
* Copyright (c) 2014 PX4 Development Team. All rights reserved.
*
@ -37,7 +37,19 @@ e/****************************************************************************
*
* @author Roman Bapst <romanbapst@yahoo.de>
*/
#include "ros/ros.h"
#include <ros/ros.h>
#include <px4.h>
#include <lib/mathlib/mathlib.h>
#include <mav_msgs/MotorSpeed.h>
#define _rotor_count 4
struct Rotor {
float roll_scale;
float pitch_scale;
float yaw_scale;
};
struct {
float control[8];
@ -47,16 +59,96 @@ e/****************************************************************************
float control[8];
}outputs;
void mix(void *input) {
const Rotor _config_x[] = {
{ 0.000000, -1.000000, -1.00 },
{ -0.000000, 1.000000, -1.00 },
{ 1.000000, 0.000000, 1.00 },
{ -1.000000, 0.000000, 1.00 },
};
const Rotor *_rotors = { &_config_x[0]
};
void mix() {
float roll = math::constrain(inputs.control[0], -1.0f, 1.0f);
float pitch = math::constrain(inputs.control[1], -1.0f, 1.0f);
float yaw = math::constrain(inputs.control[2], -1.0f, 1.0f);
float thrust = math::constrain(inputs.control[3], 0.0f, 1.0f);
float min_out = 0.0f;
float max_out = 0.0f;
/* perform initial mix pass yielding unbounded outputs, ignore yaw */
for (unsigned i = 0; i < _rotor_count; i++) {
float out = roll * _rotors[i].roll_scale
+ pitch * _rotors[i].pitch_scale + thrust;
/* limit yaw if it causes outputs clipping */
if (out >= 0.0f && out < -yaw * _rotors[i].yaw_scale) {
yaw = -out / _rotors[i].yaw_scale;
}
/* calculate min and max output values */
if (out < min_out) {
min_out = out;
}
if (out > max_out) {
max_out = out;
}
outputs.control[i] = out;
}
/* scale down roll/pitch controls if some outputs are negative, don't add yaw, keep total thrust */
if (min_out < 0.0f) {
float scale_in = thrust / (thrust - min_out);
/* mix again with adjusted controls */
for (unsigned i = 0; i < _rotor_count; i++) {
outputs.control[i] = scale_in
* (roll * _rotors[i].roll_scale
+ pitch * _rotors[i].pitch_scale) + thrust;
}
} else {
/* roll/pitch mixed without limiting, add yaw control */
for (unsigned i = 0; i < _rotor_count; i++) {
outputs.control[i] += yaw * _rotors[i].yaw_scale;
}
}
/* scale down all outputs if some outputs are too large, reduce total thrust */
float scale_out;
if (max_out > 1.0f) {
scale_out = 1.0f / max_out;
} else {
scale_out = 1.0f;
}
/* scale outputs to range _idle_speed..1, and do final limiting */
for (unsigned i = 0; i < _rotor_count; i++) {
outputs.control[i] = math::constrain(outputs.control[i], 0.0f, 1.0f);
}
}
void actuatorControlsCallback(const PX4_TOPIC_T(actuator_controls_0) &msg)
{
// read message
memcpy(inputs,msg,sizeof(inputs));
for(int i = 0;i < msg.NUM_ACTUATOR_CONTROLS;i++) {
inputs.control[i] = msg.control[i];
}
// mix
mix();
// publish message
mav_msgs::MotorSpeed rotor_vel_msg;
for (int i = 0; i < _rotor_count; i++) {
rotor_vel_msg.motor_speed.push_back(outputs.control[i]);
}
pub.publish(rotor_vel_msg);
}
@ -65,6 +157,7 @@ void mix(void *input) {
ros::init(argc, argv, "mc_mixer");
ros::NodeHandle n;
ros::Subscriber sub = n.subscribe("actuator_controls_0", 1000, actuatorControlsCallback);
ros::Publisher pub = n.advertise<mav_msgs::MotorSpeed>("mixed_motor_commands",10);
ros::spin();