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143 lines
5.3 KiB
C++
143 lines
5.3 KiB
C++
/****************************************************************************
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*
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* Copyright (c) 2017 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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*
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* This module is a modification of the fixed wing module and it is designed for ground rovers.
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* It has been developed starting from the fw module, simplified and improved with dedicated items.
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*
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* All the acknowledgments and credits for the fw wing app are reported in those files.
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*
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* @author Marco Zorzi <mzorzi@student.ethz.ch>
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*/
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#include <px4_config.h>
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#include <px4_defines.h>
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#include <px4_tasks.h>
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#include <px4_posix.h>
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#include <drivers/drv_hrt.h>
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#include <mathlib/mathlib.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/perf_counter.h>
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#include <uORB/topics/actuator_controls.h>
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#include <uORB/topics/battery_status.h>
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#include <uORB/topics/manual_control_setpoint.h>
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#include <uORB/topics/parameter_update.h>
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#include <uORB/topics/vehicle_attitude.h>
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#include <uORB/topics/vehicle_attitude_setpoint.h>
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#include <uORB/topics/vehicle_control_mode.h>
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#include <uORB/topics/vehicle_rates_setpoint.h>
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#include <uORB/uORB.h>
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using matrix::Eulerf;
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using matrix::Quatf;
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class GroundRoverAttitudeControl
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{
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public:
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GroundRoverAttitudeControl();
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~GroundRoverAttitudeControl();
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int start();
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bool task_running() { return _task_running; }
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private:
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bool _task_should_exit{false}; /**< if true, attitude control task should exit */
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bool _task_running{false}; /**< if true, task is running in its mainloop */
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int _control_task{-1}; /**< task handle */
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int _att_sp_sub{-1}; /**< vehicle attitude setpoint */
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int _battery_status_sub{-1}; /**< battery status subscription */
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int _att_sub{-1}; /**< control state subscription */
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int _manual_sub{-1}; /**< notification of manual control updates */
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int _params_sub{-1}; /**< notification of parameter updates */
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int _vcontrol_mode_sub{-1}; /**< vehicle status subscription */
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orb_advert_t _actuators_0_pub{nullptr}; /**< actuator control group 0 setpoint */
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actuator_controls_s _actuators {}; /**< actuator control inputs */
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battery_status_s _battery_status {}; /**< battery status */
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manual_control_setpoint_s _manual {}; /**< r/c channel data */
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vehicle_attitude_s _att {}; /**< control state */
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vehicle_attitude_setpoint_s _att_sp {}; /**< vehicle attitude setpoint */
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vehicle_control_mode_s _vcontrol_mode {}; /**< vehicle control mode */
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perf_counter_t _loop_perf; /**< loop performance counter */
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perf_counter_t _nonfinite_input_perf; /**< performance counter for non finite input */
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perf_counter_t _nonfinite_output_perf; /**< performance counter for non finite output */
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bool _debug{false}; /**< if set to true, print debug output */
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struct {
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float w_p; /**< Proportional gain of the steering controller */
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float w_i; /**< Integral gain of the steering controller */
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float w_d; /**< Derivative of the steering controller */
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float w_imax; /**< maximum integrator level of the steering controller */
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float trim_yaw;
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float man_yaw_scale; /**< scale factor applied to yaw actuator control in pure manual mode */
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int32_t bat_scale_en; /**< Battery scaling enabled */
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} _parameters{}; /**< local copies of interesting parameters */
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struct {
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param_t w_p;
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param_t w_i;
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param_t w_d;
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param_t w_imax;
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param_t trim_yaw;
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param_t man_yaw_scale;
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param_t bat_scale_en;
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} _parameter_handles{}; /**< handles for interesting parameters */
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PID_t _steering_ctrl{};
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void parameters_update();
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void vehicle_control_mode_poll();
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void manual_control_setpoint_poll();
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void vehicle_attitude_setpoint_poll();
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void battery_status_poll();
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static void task_main_trampoline(int argc, char *argv[]);
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void task_main();
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};
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