removed secondary attitude from attitude topic

src/modules/uORB/topics/vehicle_attitude.h

@@ -79,24 +79,6 @@ struct vehicle_attitude_s {
 	float g_comp[3];	/**< Compensated gravity vector					*/
 	bool R_valid;		/**< Rotation matrix valid					*/
 	bool q_valid;		/**< Quaternion valid						*/
-
-	// secondary attitude, use for VTOL
-	float roll_sec;		/**< Roll angle (rad, Tait-Bryan, NED)				*/
-	float pitch_sec;		/**< Pitch angle (rad, Tait-Bryan, NED)				*/
-	float yaw_sec;		/**< Yaw angle (rad, Tait-Bryan, NED)				*/
-	float rollspeed_sec;	/**< Roll angular speed (rad/s, Tait-Bryan, NED)		*/
-	float pitchspeed_sec;	/**< Pitch angular speed (rad/s, Tait-Bryan, NED)		*/
-	float yawspeed_sec;		/**< Yaw angular speed (rad/s, Tait-Bryan, NED)			*/
-	float rollacc_sec;		/**< Roll angular accelration (rad/s, Tait-Bryan, NED)		*/
-	float pitchacc_sec;		/**< Pitch angular acceleration (rad/s, Tait-Bryan, NED)	*/
-	float yawacc_sec;		/**< Yaw angular acceleration (rad/s, Tait-Bryan, NED)		*/
-	float rate_offsets_sec[3];	/**< Offsets of the body angular rates from zero		*/
-	float R_sec[3][3];		/**< Rotation matrix body to world, (Tait-Bryan, NED)		*/
-	float q_sec[4];		/**< Quaternion (NED)						*/
-	float g_comp_sec[3];	/**< Compensated gravity vector					*/
-	bool R_valid_sec;		/**< Rotation matrix valid					*/
-	bool q_valid_sec;		/**< Quaternion valid						*/
-
 };
 
 /**