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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
+
+using namespace px4;
+
+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::Subscriber<px4_vehicle_attitude> *_v_att; /**< vehicle attitude */
+ px4::Subscriber<px4_vehicle_attitude_setpoint> *_v_att_sp; /**< vehicle attitude setpoint */
+ px4::Subscriber<px4_vehicle_rates_setpoint> *_v_rates_sp; /**< vehicle rates setpoint */
+ px4::Subscriber<px4_vehicle_control_mode> *_v_control_mode; /**< vehicle control mode */
+ px4::Subscriber<px4_parameter_update> *_parameter_update; /**< parameter update */
+ px4::Subscriber<px4_manual_control_setpoint> *_manual_control_sp; /**< manual control setpoint */
+ px4::Subscriber<px4_actuator_armed> *_armed; /**< actuator arming status */
+ px4::Subscriber<px4_vehicle_status> *_v_status; /**< vehicle status */
+
+ px4_vehicle_attitude_setpoint _v_att_sp_mod; /**< modified vehicle attitude setpoint
+ that gets published eventually */
+ px4_vehicle_rates_setpoint _v_rates_sp_mod; /**< vehicle rates setpoint
+ that gets published eventually*/
+ px4_actuator_controls_0 _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_ */