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move vehicle_attitude_setpoint to msg format
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@@ -1,7 +1,6 @@
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/****************************************************************************
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*
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* Copyright (C) 2012 PX4 Development Team. All rights reserved.
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* Author: @author Lorenz Meier <lm@inf.ethz.ch>
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* Copyright (C) 2013-2014 PX4 Development Team. All rights reserved.
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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@@ -32,49 +31,37 @@
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*
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****************************************************************************/
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/**
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* @file vehicle_attitude_setpoint.h
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* Definition of the vehicle attitude setpoint uORB topic.
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*/
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/* Auto-generated by genmsg_cpp from file /home/thomasgubler/src/catkin_ws/src/Firmware/msg/px4_msgs/vehicle_attitude_setpoint.msg */
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#ifndef TOPIC_VEHICLE_ATTITUDE_SETPOINT_H_
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#define TOPIC_VEHICLE_ATTITUDE_SETPOINT_H_
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#pragma once
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#include <stdint.h>
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#include <stdbool.h>
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#include <platforms/px4_defines.h>
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#include "../uORB.h"
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/**
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* @addtogroup topics
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* @{
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*/
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/**
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* vehicle attitude setpoint.
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*/
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struct vehicle_attitude_setpoint_s {
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uint64_t timestamp; /**< in microseconds since system start, is set whenever the writing thread stores new data */
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float roll_body; /**< body angle in NED frame */
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float pitch_body; /**< body angle in NED frame */
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float yaw_body; /**< body angle in NED frame */
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//float body_valid; /**< Set to true if body angles are valid */
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float R_body[3][3]; /**< Rotation matrix describing the setpoint as rotation from the current body frame */
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bool R_valid; /**< Set to true if rotation matrix is valid */
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//! For quaternion-based attitude control
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float q_d[4]; /** Desired quaternion for quaternion control */
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bool q_d_valid; /**< Set to true if quaternion vector is valid */
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float q_e[4]; /** Attitude error in quaternion */
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bool q_e_valid; /**< Set to true if quaternion error vector is valid */
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float thrust; /**< Thrust in Newton the power system should generate */
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bool roll_reset_integral; /**< Reset roll integral part (navigation logic change) */
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bool pitch_reset_integral; /**< Reset pitch integral part (navigation logic change) */
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bool yaw_reset_integral; /**< Reset yaw integral part (navigation logic change) */
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uint64_t timestamp;
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float roll_body;
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float pitch_body;
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float yaw_body;
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float R_body[9];
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bool R_valid;
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float q_d[4];
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bool q_d_valid;
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float q_e[4];
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bool q_e_valid;
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float thrust;
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bool roll_reset_integral;
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bool pitch_reset_integral;
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bool yaw_reset_integral;
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};
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/**
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@@ -83,5 +70,3 @@ struct vehicle_attitude_setpoint_s {
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/* register this as object request broker structure */
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ORB_DECLARE(vehicle_attitude_setpoint);
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#endif /* TOPIC_ARDRONE_CONTROL_H_ */
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