forked from Archive/PX4-Autopilot
298 lines
8.9 KiB
C
298 lines
8.9 KiB
C
/****************************************************************************
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*
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* Copyright (C) 2012 PX4 Development Team. All rights reserved.
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* Author: @author Thomas Gubler <thomasgubler@student.ethz.ch>
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* @author Doug Weibel <douglas.weibel@colorado.edu>
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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 fixedwing_att_control.c
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* Implementation of a fixed wing attitude controller.
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*/
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#include <nuttx/config.h>
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#include <stdio.h>
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#include <stdlib.h>
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#include <string.h>
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#include <unistd.h>
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#include <fcntl.h>
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#include <errno.h>
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#include <math.h>
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#include <poll.h>
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#include <time.h>
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#include <drivers/drv_hrt.h>
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#include <arch/board/board.h>
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#include <uORB/uORB.h>
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#include <uORB/topics/vehicle_global_position.h>
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#include <uORB/topics/vehicle_global_position_setpoint.h>
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#include <uORB/topics/vehicle_attitude.h>
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#include <uORB/topics/vehicle_status.h>
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#include <uORB/topics/vehicle_attitude_setpoint.h>
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#include <uORB/topics/manual_control_setpoint.h>
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#include <uORB/topics/actuator_controls.h>
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#include <uORB/topics/vehicle_rates_setpoint.h>
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#include <uORB/topics/debug_key_value.h>
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#include <systemlib/param/param.h>
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#include <systemlib/pid/pid.h>
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#include <systemlib/geo/geo.h>
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#include <systemlib/systemlib.h>
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#include <fixedwing_att_control_rate.h>
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#include <fixedwing_att_control_att.h>
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/*
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* Controller parameters, accessible via MAVLink
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*
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*/
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// Roll control parameters
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PARAM_DEFINE_FLOAT(FW_ROLLR_P, 0.9f);
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PARAM_DEFINE_FLOAT(FW_ROLLR_I, 0.2f);
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PARAM_DEFINE_FLOAT(FW_ROLLR_AWU, 0.9f);
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PARAM_DEFINE_FLOAT(FW_ROLLR_LIM, 0.7f); // Roll rate limit in radians/sec, applies to the roll controller
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PARAM_DEFINE_FLOAT(FW_ROLL_P, 4.0f);
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PARAM_DEFINE_FLOAT(FW_PITCH_RCOMP, 0.1f);
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//Pitch control parameters
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PARAM_DEFINE_FLOAT(FW_PITCHR_P, 0.8f);
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PARAM_DEFINE_FLOAT(FW_PITCHR_I, 0.2f);
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PARAM_DEFINE_FLOAT(FW_PITCHR_AWU, 0.8f);
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PARAM_DEFINE_FLOAT(FW_PITCHR_LIM, 0.35f); // Pitch rate limit in radians/sec, applies to the pitch controller
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PARAM_DEFINE_FLOAT(FW_PITCH_P, 8.0f);
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//Yaw control parameters //XXX TODO this is copy paste, asign correct values
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PARAM_DEFINE_FLOAT(FW_YAWR_P, 0.3f);
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PARAM_DEFINE_FLOAT(FW_YAWR_I, 0.0f);
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PARAM_DEFINE_FLOAT(FW_YAWR_AWU, 0.0f);
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PARAM_DEFINE_FLOAT(FW_YAWR_LIM, 0.35f); // Yaw rate limit in radians/sec
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/* Prototypes */
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/**
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* Deamon management function.
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*/
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__EXPORT int fixedwing_att_control_main(int argc, char *argv[]);
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/**
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* Mainloop of deamon.
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*/
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int fixedwing_att_control_thread_main(int argc, char *argv[]);
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/**
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* Print the correct usage.
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*/
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static void usage(const char *reason);
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/* Variables */
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static bool thread_should_exit = false; /**< Deamon exit flag */
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static bool thread_running = false; /**< Deamon status flag */
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static int deamon_task; /**< Handle of deamon task / thread */
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/* Main Thread */
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int fixedwing_att_control_thread_main(int argc, char *argv[])
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{
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/* read arguments */
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bool verbose = false;
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for (int i = 1; i < argc; i++) {
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if (strcmp(argv[i], "-v") == 0 || strcmp(argv[i], "--verbose") == 0) {
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verbose = true;
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}
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}
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/* welcome user */
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printf("[fixedwing att_control] started\n");
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/* declare and safely initialize all structs */
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struct vehicle_attitude_s att;
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memset(&att, 0, sizeof(att));
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struct vehicle_attitude_setpoint_s att_sp;
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memset(&att_sp, 0, sizeof(att_sp));
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struct vehicle_rates_setpoint_s rates_sp;
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memset(&rates_sp, 0, sizeof(rates_sp));
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struct manual_control_setpoint_s manual_sp;
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memset(&manual_sp, 0, sizeof(manual_sp));
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struct vehicle_status_s vstatus;
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memset(&vstatus, 0, sizeof(vstatus));
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// static struct debug_key_value_s debug_output;
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// memset(&debug_output, 0, sizeof(debug_output));
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/* output structs */
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struct actuator_controls_s actuators;
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memset(&actuators, 0, sizeof(actuators));
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/* publish actuator controls */
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for (unsigned i = 0; i < NUM_ACTUATOR_CONTROLS; i++) {
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actuators.control[i] = 0.0f;
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}
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orb_advert_t actuator_pub = orb_advertise(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, &actuators);
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// orb_advert_t debug_pub = orb_advertise(ORB_ID(debug_key_value), &debug_output);
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// debug_output.key[0] = '1';
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/* subscribe */
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int att_sub = orb_subscribe(ORB_ID(vehicle_attitude));
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int att_sp_sub = orb_subscribe(ORB_ID(vehicle_attitude_setpoint));
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int manual_sp_sub = orb_subscribe(ORB_ID(manual_control_setpoint));
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int vstatus_sub = orb_subscribe(ORB_ID(vehicle_status));
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/* Setup of loop */
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float gyro[3] = {0.0f, 0.0f, 0.0f};
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struct pollfd fds = { .fd = att_sub, .events = POLLIN };
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while(!thread_should_exit)
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{
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/* wait for a sensor update, check for exit condition every 500 ms */
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poll(&fds, 1, 500);
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/* get a local copy of attitude */
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orb_copy(ORB_ID(vehicle_attitude), att_sub, &att);
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orb_copy(ORB_ID(vehicle_attitude_setpoint), att_sp_sub, &att_sp);
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orb_copy(ORB_ID(manual_control_setpoint), manual_sp_sub, &manual_sp);
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orb_copy(ORB_ID(vehicle_status), vstatus_sub, &vstatus);
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gyro[0] = att.rollspeed;
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gyro[1] = att.pitchspeed;
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gyro[2] = att.yawspeed;
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/* Control */
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if (vstatus.state_machine == SYSTEM_STATE_AUTO) {
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/* Attitude Control */
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fixedwing_att_control_attitude(&att_sp,
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&att,
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&rates_sp);
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/* Attitude Rate Control */
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fixedwing_att_control_rates(&rates_sp, gyro, &actuators);
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//REMOVEME XXX
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actuators.control[3] = 0.7f;
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// debug_output.value = rates_sp.pitch;
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// orb_publish(ORB_ID(debug_key_value), debug_pub, &debug_output);
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} else if (vstatus.state_machine == SYSTEM_STATE_MANUAL) {
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/* directly pass through values */
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actuators.control[0] = manual_sp.roll;
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/* positive pitch means negative actuator -> pull up */
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actuators.control[1] = -manual_sp.pitch;
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actuators.control[2] = manual_sp.yaw;
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actuators.control[3] = manual_sp.throttle;
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}
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/* publish output */
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orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators);
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}
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printf("[fixedwing_att_control] exiting, stopping all motors.\n");
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thread_running = false;
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/* kill all outputs */
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for (unsigned i = 0; i < NUM_ACTUATOR_CONTROLS; i++)
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actuators.control[i] = 0.0f;
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orb_publish(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_pub, &actuators);
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close(att_sub);
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close(actuator_pub);
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fflush(stdout);
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exit(0);
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return 0;
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}
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/* Startup Functions */
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static void
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usage(const char *reason)
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{
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if (reason)
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fprintf(stderr, "%s\n", reason);
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fprintf(stderr, "usage: fixedwing_att_control {start|stop|status}\n\n");
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exit(1);
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}
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/**
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* The deamon app only briefly exists to start
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* the background job. The stack size assigned in the
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* Makefile does only apply to this management task.
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*
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* The actual stack size should be set in the call
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* to task_create().
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*/
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int fixedwing_att_control_main(int argc, char *argv[])
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{
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if (argc < 1)
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usage("missing command");
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if (!strcmp(argv[1], "start")) {
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if (thread_running) {
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printf("fixedwing_att_control already running\n");
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/* this is not an error */
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exit(0);
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}
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thread_should_exit = false;
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deamon_task = task_spawn("fixedwing_att_control",
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SCHED_DEFAULT,
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SCHED_PRIORITY_MAX - 20,
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4096,
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fixedwing_att_control_thread_main,
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(argv) ? (const char **)&argv[2] : (const char **)NULL);
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thread_running = true;
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exit(0);
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}
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if (!strcmp(argv[1], "stop")) {
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thread_should_exit = true;
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exit(0);
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}
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if (!strcmp(argv[1], "status")) {
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if (thread_running) {
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printf("\tfixedwing_att_control is running\n");
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} else {
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printf("\tfixedwing_att_control not started\n");
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}
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exit(0);
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}
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usage("unrecognized command");
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exit(1);
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}
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