/****************************************************************************
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 *   Copyright (C) 2008-2012 PX4 Development Team. All rights reserved.
 *   Author: @author Thomas Gubler <thomasgubler@student.ethz.ch>
 *           @author Julian Oes <joes@student.ethz.ch>
 *           @author Lorenz Meier <lm@inf.ethz.ch>
 *
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 *
 * 1. Redistributions of source code must retain the above copyright
 *    notice, this list of conditions and the following disclaimer.
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 *    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
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 *
 * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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/**
 * @file vehicle_attitude.h
 * Definition of the attitude uORB topic.
 */

#ifndef VEHICLE_ATTITUDE_H_
#define VEHICLE_ATTITUDE_H_

#include <stdint.h>
#include <stdbool.h>
#include "../uORB.h"

/**
 * @addtogroup topics
 */

/**
 * Attitude in NED body frame in SI units.
 *
 * @see http://en.wikipedia.org/wiki/International_System_of_Units
 */
struct vehicle_attitude_s {

	uint64_t timestamp;	/**< in microseconds since system start          */

	/* This is similar to the mavlink message ATTITUDE, but for onboard use */

	/** @warning roll, pitch and yaw have always to be valid, the rotation matrix and quaternion are optional */

	float roll;		/**< Roll angle (rad, Tait-Bryan, NED)				*/
	float pitch;		/**< Pitch angle (rad, Tait-Bryan, NED)				*/
	float yaw;		/**< Yaw angle (rad, Tait-Bryan, NED)				*/
	float rollspeed;	/**< Roll angular speed (rad/s, Tait-Bryan, NED)		*/
	float pitchspeed;	/**< Pitch angular speed (rad/s, Tait-Bryan, NED)		*/
	float yawspeed;		/**< Yaw angular speed (rad/s, Tait-Bryan, NED)			*/
	float rollacc;		/**< Roll angular accelration (rad/s, Tait-Bryan, NED)		*/
	float pitchacc;		/**< Pitch angular acceleration (rad/s, Tait-Bryan, NED)	*/
	float yawacc;		/**< Yaw angular acceleration (rad/s, Tait-Bryan, NED)		*/
	float rate_offsets[3];	/**< Offsets of the body angular rates from zero		*/
	float R[3][3];		/**< Rotation matrix body to world, (Tait-Bryan, NED)		*/
	float q[4];		/**< Quaternion (NED)						*/
	bool R_valid;		/**< Rotation matrix valid					*/
	bool q_valid;		/**< Quaternion valid						*/

};

/**
 * @}
 */

/* register this as object request broker structure */
ORB_DECLARE(vehicle_attitude);

#endif
