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-rw-r--r--src/modules/uORB/topics/vehicle_attitude_setpoint.h59
1 files changed, 22 insertions, 37 deletions
diff --git a/src/modules/uORB/topics/vehicle_attitude_setpoint.h b/src/modules/uORB/topics/vehicle_attitude_setpoint.h
index a503aa0c6..29fb104df 100644
--- a/src/modules/uORB/topics/vehicle_attitude_setpoint.h
+++ b/src/modules/uORB/topics/vehicle_attitude_setpoint.h
@@ -1,7 +1,6 @@
/****************************************************************************
*
- * Copyright (C) 2012 PX4 Development Team. All rights reserved.
- * Author: @author Lorenz Meier <lm@inf.ethz.ch>
+ * Copyright (C) 2013-2014 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
@@ -32,49 +31,37 @@
*
****************************************************************************/
-/**
- * @file vehicle_attitude_setpoint.h
- * Definition of the vehicle attitude setpoint uORB topic.
- */
+ /* Auto-generated by genmsg_cpp from file /home/thomasgubler/src/catkin_ws/src/Firmware/msg/px4_msgs/vehicle_attitude_setpoint.msg */
-#ifndef TOPIC_VEHICLE_ATTITUDE_SETPOINT_H_
-#define TOPIC_VEHICLE_ATTITUDE_SETPOINT_H_
+
+#pragma once
#include <stdint.h>
-#include <stdbool.h>
-#include <platforms/px4_defines.h>
+#include "../uORB.h"
+
+
/**
* @addtogroup topics
* @{
*/
-/**
- * vehicle attitude setpoint.
- */
-struct vehicle_attitude_setpoint_s {
- uint64_t timestamp; /**< in microseconds since system start, is set whenever the writing thread stores new data */
-
- float roll_body; /**< body angle in NED frame */
- float pitch_body; /**< body angle in NED frame */
- float yaw_body; /**< body angle in NED frame */
- //float body_valid; /**< Set to true if body angles are valid */
-
- float R_body[3][3]; /**< Rotation matrix describing the setpoint as rotation from the current body frame */
- bool R_valid; /**< Set to true if rotation matrix is valid */
-
- //! For quaternion-based attitude control
- float q_d[4]; /** Desired quaternion for quaternion control */
- bool q_d_valid; /**< Set to true if quaternion vector is valid */
- float q_e[4]; /** Attitude error in quaternion */
- bool q_e_valid; /**< Set to true if quaternion error vector is valid */
-
- float thrust; /**< Thrust in Newton the power system should generate */
-
- bool roll_reset_integral; /**< Reset roll integral part (navigation logic change) */
- bool pitch_reset_integral; /**< Reset pitch integral part (navigation logic change) */
- bool yaw_reset_integral; /**< Reset yaw integral part (navigation logic change) */
+struct vehicle_attitude_setpoint_s {
+ uint64_t timestamp;
+ float roll_body;
+ float pitch_body;
+ float yaw_body;
+ float R_body[9];
+ bool R_valid;
+ float q_d[4];
+ bool q_d_valid;
+ float q_e[4];
+ bool q_e_valid;
+ float thrust;
+ bool roll_reset_integral;
+ bool pitch_reset_integral;
+ bool yaw_reset_integral;
};
/**
@@ -83,5 +70,3 @@ struct vehicle_attitude_setpoint_s {
/* register this as object request broker structure */
ORB_DECLARE(vehicle_attitude_setpoint);
-
-#endif /* TOPIC_ARDRONE_CONTROL_H_ */