Merge branch 'beta_mavlink2' into mpc_local_pos_mavlink

src/modules/uORB/topics/mission_result.h

@@ -54,7 +54,8 @@
 struct mission_result_s
 {
 	bool mission_reached;		/**< true if mission has been reached			*/
-	unsigned mission_index;		/**< index of the mission which has been reached	*/
+	unsigned mission_index_reached;	/**< index of the mission which has been reached	*/
+	unsigned index_current_mission; /**< index of the current mission			*/
 };
 
 /**

src/modules/uORB/topics/sensor_combined.h

@@ -77,34 +77,33 @@ struct sensor_combined_s {
 
 	/* NOTE: Ordering of fields optimized to align to 32 bit / 4 bytes Change with consideration only   */
 
-	uint64_t timestamp;			/**< Timestamp in microseconds since boot         */
+	uint64_t timestamp;			/**< Timestamp in microseconds since boot, from gyro         */
 
 	int16_t	gyro_raw[3];			/**< Raw sensor values of angular velocity        */
-	uint16_t gyro_counter;			/**< Number of raw measurments taken              */
 	float gyro_rad_s[3];			/**< Angular velocity in radian per seconds       */
-	
+
 	int16_t accelerometer_raw[3];		/**< Raw acceleration in NED body frame           */
-	uint32_t accelerometer_counter;		/**< Number of raw acc measurements taken         */
 	float accelerometer_m_s2[3];		/**< Acceleration in NED body frame, in m/s^2     */
 	int accelerometer_mode;			/**< Accelerometer measurement mode */
 	float accelerometer_range_m_s2;		/**< Accelerometer measurement range in m/s^2 */
+	uint64_t accelerometer_timestamp;	/**< Accelerometer timestamp        */
 
 	int16_t	magnetometer_raw[3];		/**< Raw magnetic field in NED body frame         */
 	float magnetometer_ga[3];		/**< Magnetic field in NED body frame, in Gauss   */
 	int magnetometer_mode;			/**< Magnetometer measurement mode */
 	float magnetometer_range_ga;		/**< ± measurement range in Gauss */
 	float magnetometer_cuttoff_freq_hz;	/**< Internal analog low pass frequency of sensor */
-	uint32_t magnetometer_counter;		/**< Number of raw mag measurements taken         */
-	
+	uint64_t magnetometer_timestamp;	/**< Magnetometer timestamp         */
+
 	float baro_pres_mbar;			/**< Barometric pressure, already temp. comp.     */
 	float baro_alt_meter;			/**< Altitude, already temp. comp.                */
 	float baro_temp_celcius;		/**< Temperature in degrees celsius               */
 	float adc_voltage_v[4];			/**< ADC voltages of ADC Chan 10/11/12/13 or -1      */
 	float mcu_temp_celcius;			/**< Internal temperature measurement of MCU */
-	uint32_t baro_counter;			/**< Number of raw baro measurements taken        */
+	uint64_t baro_timestamp;		/**< Barometer timestamp        */
 
-	float differential_pressure_pa;				/**< Airspeed sensor differential pressure                  */ 
-	uint32_t differential_pressure_counter;		/**< Number of raw differential pressure measurements taken */
+	float differential_pressure_pa;				/**< Airspeed sensor differential pressure                  */
+	uint64_t differential_pressure_timestamp;		/**< Last measurement timestamp */
 };
 
 /**

src/modules/uORB/topics/vehicle_attitude.h

@@ -76,7 +76,7 @@ struct vehicle_attitude_s {
 	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)						*/
-	float g_comp[3];	/**< Compensated gravity vector				*/
+	float g_comp[3];	/**< Compensated gravity vector					*/
 	bool R_valid;		/**< Rotation matrix valid					*/
 	bool q_valid;		/**< Quaternion valid						*/