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-rw-r--r--src/modules/mc_att_control/mc_att_control_base.h134
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diff --git a/src/modules/mc_att_control/mc_att_control_base.h b/src/modules/mc_att_control/mc_att_control_base.h
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--- a/src/modules/mc_att_control/mc_att_control_base.h
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-#ifndef MC_ATT_CONTROL_BASE_H_
-#define MC_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 mc_att_control_base.h
- *
- * MC Attitude Controller : Control and math code
- *
- * @author Tobias Naegeli <naegelit@student.ethz.ch>
- * @author Lorenz Meier <lm@inf.ethz.ch>
- * @author Anton Babushkin <anton.babushkin@me.com>
- * @author Thomas Gubler <thomasgubler@gmail.com>
- * @author Julian Oes <julian@oes.ch>
- * @author Roman Bapst <bapstr@ethz.ch>
- *
- */
-#include <px4.h>
-#include <stdio.h>
-#include <stdlib.h>
-#include <string.h>
-#include <unistd.h>
-#include <errno.h>
-#include <math.h>
-
-#include <systemlib/perf_counter.h>
-#include <lib/mathlib/mathlib.h>
-
-
-
-#define YAW_DEADZONE 0.05f
-#define MIN_TAKEOFF_THRUST 0.2f
-#define RATES_I_LIMIT 0.3f
-
-class MulticopterAttitudeControlBase
-{
-public:
- /**
- * Constructor
- */
- MulticopterAttitudeControlBase();
-
- /**
- * Destructor
- */
- ~MulticopterAttitudeControlBase();
-
- /**
- * Start the sensors task.
- *
- * @return OK on success.
- */
- void control_attitude(float dt);
- void control_attitude_rates(float dt);
-
- void set_actuator_controls();
-
-protected:
- px4::PX4_SUBSCRIBER(vehicle_attitude) *_v_att; /**< vehicle attitude */
- px4::PX4_SUBSCRIBER(vehicle_attitude_setpoint) *_v_att_sp; /**< vehicle attitude setpoint */
- px4::PX4_SUBSCRIBER(vehicle_rates_setpoint) *_v_rates_sp; /**< vehicle rates setpoint */
- px4::PX4_SUBSCRIBER(vehicle_control_mode) *_v_control_mode; /**< vehicle control mode */
- px4::PX4_SUBSCRIBER(parameter_update) *_parameter_update; /**< parameter update */
- px4::PX4_SUBSCRIBER(manual_control_setpoint) *_manual_control_sp; /**< manual control setpoint */
- px4::PX4_SUBSCRIBER(actuator_armed) *_armed; /**< actuator arming status */
- px4::PX4_SUBSCRIBER(vehicle_status) *_v_status; /**< vehicle status */
-
- PX4_TOPIC_T(vehicle_attitude_setpoint) _v_att_sp_mod; /**< modified vehicle attitude setpoint
- that gets published eventually */
- PX4_TOPIC_T(vehicle_rates_setpoint) _v_rates_sp_mod; /**< vehicle rates setpoint
- that gets published eventually*/
- PX4_TOPIC_T(actuator_controls) _actuators; /**< actuator controls */
-
- math::Vector<3> _rates_prev; /**< angular rates on previous step */
- math::Vector<3> _rates_sp; /**< angular rates setpoint */
- math::Vector<3> _rates_int; /**< angular rates integral error */
- float _thrust_sp; /**< thrust setpoint */
- math::Vector<3> _att_control; /**< attitude control vector */
-
- math::Matrix<3, 3> _I; /**< identity matrix */
-
- bool _reset_yaw_sp; /**< reset yaw setpoint flag */
-
- struct {
- math::Vector<3> att_p; /**< P gain for angular error */
- math::Vector<3> rate_p; /**< P gain for angular rate error */
- math::Vector<3> rate_i; /**< I gain for angular rate error */
- math::Vector<3> rate_d; /**< D gain for angular rate error */
- float yaw_ff; /**< yaw control feed-forward */
- float yaw_rate_max; /**< max yaw rate */
-
- float man_roll_max;
- float man_pitch_max;
- float man_yaw_max;
- math::Vector<3> acro_rate_max; /**< max attitude rates in acro mode */
-
- int32_t autostart_id;
- } _params;
-
- bool _publish_att_sp;
-
-};
-
-#endif /* MC_ATT_CONTROL_BASE_H_ */