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+#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_ */