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-rw-r--r--src/modules/fw_att_control/fw_att_control_base.h151
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diff --git a/src/modules/fw_att_control/fw_att_control_base.h b/src/modules/fw_att_control/fw_att_control_base.h
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--- a/src/modules/fw_att_control/fw_att_control_base.h
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@@ -1,151 +0,0 @@
-#ifndef FW_ATT_CONTROL_BASE_H_
-#define FW_ATT_CONTROL_BASE_H_
-
-/* Copyright (c) 2014 PX4 Development Team. All rights reserved.
-*
-* Redistribution and use in source and binary forms, with or without
-* modification, are permitted provided that the following conditions
-* are met:
-*
-* 1. Redistributions of source code must retain the above copyright
-* notice, this list of conditions and the following disclaimer.
-* 2. Redistributions in binary form must reproduce the above copyright
-* notice, this list of conditions and the following disclaimer in
-* the documentation and/or other materials provided with the
-* distribution.
-* 3. Neither the name PX4 nor the names of its contributors may be
-* used to endorse or promote products derived from this software
-* without specific prior written permission.
-*
-* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
-* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
-* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
-* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
-* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
-* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
- * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
- * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
-* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
-* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
-* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
-* POSSIBILITY OF SUCH DAMAGE.
-*
-****************************************************************************/
-
-/**
- * @file fw_att_control_base.h
- *
- * @author Roman Bapst <bapstr@ethz.ch>
- *
- */
-
-#include <ecl/attitude_fw/ecl_pitch_controller.h>
-#include <ecl/attitude_fw/ecl_roll_controller.h>
-#include <ecl/attitude_fw/ecl_yaw_controller.h>
-
-#include <uORB/topics/airspeed.h>
-#include <uORB/topics/vehicle_attitude_setpoint.h>
-#include <uORB/topics/manual_control_setpoint.h>
-#include <uORB/topics/actuator_controls.h>
-#include <uORB/topics/vehicle_rates_setpoint.h>
-#include <uORB/topics/vehicle_attitude.h>
-#include <uORB/topics/vehicle_control_mode.h>
-#include <uORB/topics/parameter_update.h>
-#include <uORB/topics/vehicle_global_position.h>
-#include <uORB/topics/vehicle_status.h>
-
-#include <systemlib/perf_counter.h>
-
-class FixedwingAttitudeControlBase
-{
-public:
- /**
- * Constructor
- */
- FixedwingAttitudeControlBase();
-
- /**
- * Destructor
- */
- ~FixedwingAttitudeControlBase();
-
-
-protected:
-
- bool _task_should_exit; /**< if true, sensor task should exit */
- bool _task_running; /**< if true, task is running in its mainloop */
- int _control_task; /**< task handle for sensor task */
-
- struct vehicle_attitude_s _att; /**< vehicle attitude */
- struct vehicle_attitude_setpoint_s _att_sp; /**< vehicle attitude setpoint */
- struct manual_control_setpoint_s _manual; /**< r/c channel data */
- struct airspeed_s _airspeed; /**< airspeed */
- struct vehicle_control_mode_s _vcontrol_mode; /**< vehicle control mode */
- struct actuator_controls_s _actuators; /**< actuator control inputs */
- struct actuator_controls_s _actuators_airframe; /**< actuator control inputs */
- struct vehicle_global_position_s _global_pos; /**< global position */
- struct vehicle_status_s _vehicle_status; /**< vehicle status */
-
- perf_counter_t _loop_perf; /**< loop performance counter */
- perf_counter_t _nonfinite_input_perf; /**< performance counter for non finite input */
- perf_counter_t _nonfinite_output_perf; /**< performance counter for non finite output */
-
- bool _setpoint_valid; /**< flag if the position control setpoint is valid */
- bool _debug; /**< if set to true, print debug output */
-
- struct {
- float tconst;
- float p_p;
- float p_d;
- float p_i;
- float p_ff;
- float p_rmax_pos;
- float p_rmax_neg;
- float p_integrator_max;
- float p_roll_feedforward;
- float r_p;
- float r_d;
- float r_i;
- float r_ff;
- float r_integrator_max;
- float r_rmax;
- float y_p;
- float y_i;
- float y_d;
- float y_ff;
- float y_roll_feedforward;
- float y_integrator_max;
- float y_coordinated_min_speed;
- float y_rmax;
-
- float airspeed_min;
- float airspeed_trim;
- float airspeed_max;
-
- float trim_roll;
- float trim_pitch;
- float trim_yaw;
- float rollsp_offset_deg; /**< Roll Setpoint Offset in deg */
- float pitchsp_offset_deg; /**< Pitch Setpoint Offset in deg */
- float rollsp_offset_rad; /**< Roll Setpoint Offset in rad */
- float pitchsp_offset_rad; /**< Pitch Setpoint Offset in rad */
- float man_roll_max; /**< Max Roll in rad */
- float man_pitch_max; /**< Max Pitch in rad */
-
- } _parameters; /**< local copies of interesting parameters */
-
- ECL_RollController _roll_ctrl;
- ECL_PitchController _pitch_ctrl;
- ECL_YawController _yaw_ctrl;
-
- void control_attitude();
-
- // setters and getters for interface with euroc-gazebo simulator
- void set_attitude(const Eigen::Quaternion<double> attitude);
- void set_attitude_rates(const Eigen::Vector3d& angular_rate);
- void set_attitude_reference(const Eigen::Vector4d& control_attitude_thrust_reference);
- void get_mixer_input(Eigen::Vector4d& motor_inputs);
-
-};
-
-#endif /* FW_ATT_CONTROL_BASE_H_ */