autogenerated headers for rev...

autogenerated headers for rev https://github.com/mavlink/mavlink/tree/b905617f3577be8a55a7e7c05d9200f726bdca25

ardupilotmega/ardupilotmega.h

@@ -79,7 +79,7 @@ typedef enum MAV_CMD
 	MAV_CMD_DO_PARACHUTE=208, /* Mission command to trigger a parachute |action (0=disable, 1=enable, 2=release, for some systems see PARACHUTE_ACTION enum, not in general message set.)| Empty| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_MOTOR_TEST=209, /* Mission command to perform motor test |motor sequence number (a number from 1 to max number of motors on the vehicle)| throttle type (0=throttle percentage, 1=PWM, 2=pilot throttle channel pass-through. See MOTOR_TEST_THROTTLE_TYPE enum)| throttle| timeout (in seconds)| Empty| Empty| Empty|  */
 	MAV_CMD_DO_INVERTED_FLIGHT=210, /* Change to/from inverted flight |inverted (0=normal, 1=inverted)| Empty| Empty| Empty| Empty| Empty| Empty|  */
-	MAV_CMD_DO_MOUNT_CONTROL_QUAT=220, /* Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1| q2 - quaternion param #2| q3 - quaternion param #3| q4 - quaternion param #4| Empty| Empty| Empty|  */
+	MAV_CMD_DO_MOUNT_CONTROL_QUAT=220, /* Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1, w (1 in null-rotation)| q2 - quaternion param #2, x (0 in null-rotation)| q3 - quaternion param #3, y (0 in null-rotation)| q4 - quaternion param #4, z (0 in null-rotation)| Empty| Empty| Empty|  */
 	MAV_CMD_DO_GUIDED_MASTER=221, /* set id of master controller |System ID| Component ID| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_GUIDED_LIMITS=222, /* set limits for external control |timeout - maximum time (in seconds) that external controller will be allowed to control vehicle. 0 means no timeout| absolute altitude min (in meters, WGS84) - if vehicle moves below this alt, the command will be aborted and the mission will continue.  0 means no lower altitude limit| absolute altitude max (in meters)- if vehicle moves above this alt, the command will be aborted and the mission will continue.  0 means no upper altitude limit| horizontal move limit (in meters, WGS84) - if vehicle moves more than this distance from it's location at the moment the command was executed, the command will be aborted and the mission will continue. 0 means no horizontal altitude limit| Empty| Empty| Empty|  */
 	MAV_CMD_DO_LAST=240, /* NOP - This command is only used to mark the upper limit of the DO commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty|  */

ardupilotmega/version.h

@@ -5,7 +5,7 @@
 #ifndef MAVLINK_VERSION_H
 #define MAVLINK_VERSION_H
 
-#define MAVLINK_BUILD_DATE "Thu Jul 24 13:45:11 2014"
+#define MAVLINK_BUILD_DATE "Thu Jul 24 16:10:13 2014"
 #define MAVLINK_WIRE_PROTOCOL_VERSION "1.0"
 #define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
  

autoquad/autoquad.h

@@ -105,7 +105,7 @@ typedef enum MAV_CMD
 	MAV_CMD_DO_FENCE_ENABLE=207, /* Mission command to enable the geofence |enable? (0=disable, 1=enable)| Empty| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_PARACHUTE=208, /* Mission command to trigger a parachute |action (0=disable, 1=enable, 2=release, for some systems see PARACHUTE_ACTION enum, not in general message set.)| Empty| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_INVERTED_FLIGHT=210, /* Change to/from inverted flight |inverted (0=normal, 1=inverted)| Empty| Empty| Empty| Empty| Empty| Empty|  */
-	MAV_CMD_DO_MOUNT_CONTROL_QUAT=220, /* Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1| q2 - quaternion param #2| q3 - quaternion param #3| q4 - quaternion param #4| Empty| Empty| Empty|  */
+	MAV_CMD_DO_MOUNT_CONTROL_QUAT=220, /* Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1, w (1 in null-rotation)| q2 - quaternion param #2, x (0 in null-rotation)| q3 - quaternion param #3, y (0 in null-rotation)| q4 - quaternion param #4, z (0 in null-rotation)| Empty| Empty| Empty|  */
 	MAV_CMD_DO_GUIDED_MASTER=221, /* set id of master controller |System ID| Component ID| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_GUIDED_LIMITS=222, /* set limits for external control |timeout - maximum time (in seconds) that external controller will be allowed to control vehicle. 0 means no timeout| absolute altitude min (in meters, WGS84) - if vehicle moves below this alt, the command will be aborted and the mission will continue.  0 means no lower altitude limit| absolute altitude max (in meters)- if vehicle moves above this alt, the command will be aborted and the mission will continue.  0 means no upper altitude limit| horizontal move limit (in meters, WGS84) - if vehicle moves more than this distance from it's location at the moment the command was executed, the command will be aborted and the mission will continue. 0 means no horizontal altitude limit| Empty| Empty| Empty|  */
 	MAV_CMD_DO_LAST=240, /* NOP - This command is only used to mark the upper limit of the DO commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty|  */

autoquad/version.h

@@ -5,7 +5,7 @@
 #ifndef MAVLINK_VERSION_H
 #define MAVLINK_VERSION_H
 
-#define MAVLINK_BUILD_DATE "Thu Jul 24 13:45:18 2014"
+#define MAVLINK_BUILD_DATE "Thu Jul 24 16:10:20 2014"
 #define MAVLINK_WIRE_PROTOCOL_VERSION "1.0"
 #define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
  

common/common.h

@@ -358,7 +358,7 @@ typedef enum MAV_CMD
 	MAV_CMD_DO_FENCE_ENABLE=207, /* Mission command to enable the geofence |enable? (0=disable, 1=enable)| Empty| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_PARACHUTE=208, /* Mission command to trigger a parachute |action (0=disable, 1=enable, 2=release, for some systems see PARACHUTE_ACTION enum, not in general message set.)| Empty| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_INVERTED_FLIGHT=210, /* Change to/from inverted flight |inverted (0=normal, 1=inverted)| Empty| Empty| Empty| Empty| Empty| Empty|  */
-	MAV_CMD_DO_MOUNT_CONTROL_QUAT=220, /* Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1| q2 - quaternion param #2| q3 - quaternion param #3| q4 - quaternion param #4| Empty| Empty| Empty|  */
+	MAV_CMD_DO_MOUNT_CONTROL_QUAT=220, /* Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1, w (1 in null-rotation)| q2 - quaternion param #2, x (0 in null-rotation)| q3 - quaternion param #3, y (0 in null-rotation)| q4 - quaternion param #4, z (0 in null-rotation)| Empty| Empty| Empty|  */
 	MAV_CMD_DO_GUIDED_MASTER=221, /* set id of master controller |System ID| Component ID| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_GUIDED_LIMITS=222, /* set limits for external control |timeout - maximum time (in seconds) that external controller will be allowed to control vehicle. 0 means no timeout| absolute altitude min (in meters, WGS84) - if vehicle moves below this alt, the command will be aborted and the mission will continue.  0 means no lower altitude limit| absolute altitude max (in meters)- if vehicle moves above this alt, the command will be aborted and the mission will continue.  0 means no upper altitude limit| horizontal move limit (in meters, WGS84) - if vehicle moves more than this distance from it's location at the moment the command was executed, the command will be aborted and the mission will continue. 0 means no horizontal altitude limit| Empty| Empty| Empty|  */
 	MAV_CMD_DO_LAST=240, /* NOP - This command is only used to mark the upper limit of the DO commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty|  */

common/mavlink_msg_attitude_quaternion.h

@@ -5,10 +5,10 @@
 typedef struct __mavlink_attitude_quaternion_t
 {
  uint32_t time_boot_ms; ///< Timestamp (milliseconds since system boot)
- float q1; ///< Quaternion component 1
- float q2; ///< Quaternion component 2
- float q3; ///< Quaternion component 3
- float q4; ///< Quaternion component 4
+ float q1; ///< Quaternion component 1, w (1 in null-rotation)
+ float q2; ///< Quaternion component 2, x (0 in null-rotation)
+ float q3; ///< Quaternion component 3, y (0 in null-rotation)
+ float q4; ///< Quaternion component 4, z (0 in null-rotation)
  float rollspeed; ///< Roll angular speed (rad/s)
  float pitchspeed; ///< Pitch angular speed (rad/s)
  float yawspeed; ///< Yaw angular speed (rad/s)
@@ -44,10 +44,10 @@ typedef struct __mavlink_attitude_quaternion_t
  * @param msg The MAVLink message to compress the data into
  *
  * @param time_boot_ms Timestamp (milliseconds since system boot)
- * @param q1 Quaternion component 1
- * @param q2 Quaternion component 2
- * @param q3 Quaternion component 3
- * @param q4 Quaternion component 4
+ * @param q1 Quaternion component 1, w (1 in null-rotation)
+ * @param q2 Quaternion component 2, x (0 in null-rotation)
+ * @param q3 Quaternion component 3, y (0 in null-rotation)
+ * @param q4 Quaternion component 4, z (0 in null-rotation)
  * @param rollspeed Roll angular speed (rad/s)
  * @param pitchspeed Pitch angular speed (rad/s)
  * @param yawspeed Yaw angular speed (rad/s)
@@ -97,10 +97,10 @@ static inline uint16_t mavlink_msg_attitude_quaternion_pack(uint8_t system_id, u
  * @param chan The MAVLink channel this message will be sent over
  * @param msg The MAVLink message to compress the data into
  * @param time_boot_ms Timestamp (milliseconds since system boot)
- * @param q1 Quaternion component 1
- * @param q2 Quaternion component 2
- * @param q3 Quaternion component 3
- * @param q4 Quaternion component 4
+ * @param q1 Quaternion component 1, w (1 in null-rotation)
+ * @param q2 Quaternion component 2, x (0 in null-rotation)
+ * @param q3 Quaternion component 3, y (0 in null-rotation)
+ * @param q4 Quaternion component 4, z (0 in null-rotation)
  * @param rollspeed Roll angular speed (rad/s)
  * @param pitchspeed Pitch angular speed (rad/s)
  * @param yawspeed Yaw angular speed (rad/s)
@@ -176,10 +176,10 @@ static inline uint16_t mavlink_msg_attitude_quaternion_encode_chan(uint8_t syste
  * @param chan MAVLink channel to send the message
  *
  * @param time_boot_ms Timestamp (milliseconds since system boot)
- * @param q1 Quaternion component 1
- * @param q2 Quaternion component 2
- * @param q3 Quaternion component 3
- * @param q4 Quaternion component 4
+ * @param q1 Quaternion component 1, w (1 in null-rotation)
+ * @param q2 Quaternion component 2, x (0 in null-rotation)
+ * @param q3 Quaternion component 3, y (0 in null-rotation)
+ * @param q4 Quaternion component 4, z (0 in null-rotation)
  * @param rollspeed Roll angular speed (rad/s)
  * @param pitchspeed Pitch angular speed (rad/s)
  * @param yawspeed Yaw angular speed (rad/s)
@@ -287,7 +287,7 @@ static inline uint32_t mavlink_msg_attitude_quaternion_get_time_boot_ms(const ma
 /**
  * @brief Get field q1 from attitude_quaternion message
  *
- * @return Quaternion component 1
+ * @return Quaternion component 1, w (1 in null-rotation)
  */
 static inline float mavlink_msg_attitude_quaternion_get_q1(const mavlink_message_t* msg)
 {
@@ -297,7 +297,7 @@ static inline float mavlink_msg_attitude_quaternion_get_q1(const mavlink_message
 /**
  * @brief Get field q2 from attitude_quaternion message
  *
- * @return Quaternion component 2
+ * @return Quaternion component 2, x (0 in null-rotation)
  */
 static inline float mavlink_msg_attitude_quaternion_get_q2(const mavlink_message_t* msg)
 {
@@ -307,7 +307,7 @@ static inline float mavlink_msg_attitude_quaternion_get_q2(const mavlink_message
 /**
  * @brief Get field q3 from attitude_quaternion message
  *
- * @return Quaternion component 3
+ * @return Quaternion component 3, y (0 in null-rotation)
  */
 static inline float mavlink_msg_attitude_quaternion_get_q3(const mavlink_message_t* msg)
 {
@@ -317,7 +317,7 @@ static inline float mavlink_msg_attitude_quaternion_get_q3(const mavlink_message
 /**
  * @brief Get field q4 from attitude_quaternion message
  *
- * @return Quaternion component 4
+ * @return Quaternion component 4, z (0 in null-rotation)
  */
 static inline float mavlink_msg_attitude_quaternion_get_q4(const mavlink_message_t* msg)
 {

common/mavlink_msg_hil_state_quaternion.h

@@ -5,7 +5,7 @@
 typedef struct __mavlink_hil_state_quaternion_t
 {
  uint64_t time_usec; ///< Timestamp (microseconds since UNIX epoch or microseconds since system boot)
- float attitude_quaternion[4]; ///< Vehicle attitude expressed as normalized quaternion
+ float attitude_quaternion[4]; ///< Vehicle attitude expressed as normalized quaternion in w, x, y, z order (with 1 0 0 0 being the null-rotation)
  float rollspeed; ///< Body frame roll / phi angular speed (rad/s)
  float pitchspeed; ///< Body frame pitch / theta angular speed (rad/s)
  float yawspeed; ///< Body frame yaw / psi angular speed (rad/s)
@@ -60,7 +60,7 @@ typedef struct __mavlink_hil_state_quaternion_t
  * @param msg The MAVLink message to compress the data into
  *
  * @param time_usec Timestamp (microseconds since UNIX epoch or microseconds since system boot)
- * @param attitude_quaternion Vehicle attitude expressed as normalized quaternion
+ * @param attitude_quaternion Vehicle attitude expressed as normalized quaternion in w, x, y, z order (with 1 0 0 0 being the null-rotation)
  * @param rollspeed Body frame roll / phi angular speed (rad/s)
  * @param pitchspeed Body frame pitch / theta angular speed (rad/s)
  * @param yawspeed Body frame yaw / psi angular speed (rad/s)
@@ -135,7 +135,7 @@ static inline uint16_t mavlink_msg_hil_state_quaternion_pack(uint8_t system_id,
  * @param chan The MAVLink channel this message will be sent over
  * @param msg The MAVLink message to compress the data into
  * @param time_usec Timestamp (microseconds since UNIX epoch or microseconds since system boot)
- * @param attitude_quaternion Vehicle attitude expressed as normalized quaternion
+ * @param attitude_quaternion Vehicle attitude expressed as normalized quaternion in w, x, y, z order (with 1 0 0 0 being the null-rotation)
  * @param rollspeed Body frame roll / phi angular speed (rad/s)
  * @param pitchspeed Body frame pitch / theta angular speed (rad/s)
  * @param yawspeed Body frame yaw / psi angular speed (rad/s)
@@ -236,7 +236,7 @@ static inline uint16_t mavlink_msg_hil_state_quaternion_encode_chan(uint8_t syst
  * @param chan MAVLink channel to send the message
  *
  * @param time_usec Timestamp (microseconds since UNIX epoch or microseconds since system boot)
- * @param attitude_quaternion Vehicle attitude expressed as normalized quaternion
+ * @param attitude_quaternion Vehicle attitude expressed as normalized quaternion in w, x, y, z order (with 1 0 0 0 being the null-rotation)
  * @param rollspeed Body frame roll / phi angular speed (rad/s)
  * @param pitchspeed Body frame pitch / theta angular speed (rad/s)
  * @param yawspeed Body frame yaw / psi angular speed (rad/s)
@@ -383,7 +383,7 @@ static inline uint64_t mavlink_msg_hil_state_quaternion_get_time_usec(const mavl
 /**
  * @brief Get field attitude_quaternion from hil_state_quaternion message
  *
- * @return Vehicle attitude expressed as normalized quaternion
+ * @return Vehicle attitude expressed as normalized quaternion in w, x, y, z order (with 1 0 0 0 being the null-rotation)
  */
 static inline uint16_t mavlink_msg_hil_state_quaternion_get_attitude_quaternion(const mavlink_message_t* msg, float *attitude_quaternion)
 {

common/mavlink_msg_sim_state.h

@@ -4,10 +4,10 @@
 
 typedef struct __mavlink_sim_state_t
 {
- float q1; ///< True attitude quaternion component 1
- float q2; ///< True attitude quaternion component 2
- float q3; ///< True attitude quaternion component 3
- float q4; ///< True attitude quaternion component 4
+ float q1; ///< True attitude quaternion component 1, w (1 in null-rotation)
+ float q2; ///< True attitude quaternion component 2, x (0 in null-rotation)
+ float q3; ///< True attitude quaternion component 3, y (0 in null-rotation)
+ float q4; ///< True attitude quaternion component 4, z (0 in null-rotation)
  float roll; ///< Attitude roll expressed as Euler angles, not recommended except for human-readable outputs
  float pitch; ///< Attitude pitch expressed as Euler angles, not recommended except for human-readable outputs
  float yaw; ///< Attitude yaw expressed as Euler angles, not recommended except for human-readable outputs
@@ -69,10 +69,10 @@ typedef struct __mavlink_sim_state_t
  * @param component_id ID of this component (e.g. 200 for IMU)
  * @param msg The MAVLink message to compress the data into
  *
- * @param q1 True attitude quaternion component 1
- * @param q2 True attitude quaternion component 2
- * @param q3 True attitude quaternion component 3
- * @param q4 True attitude quaternion component 4
+ * @param q1 True attitude quaternion component 1, w (1 in null-rotation)
+ * @param q2 True attitude quaternion component 2, x (0 in null-rotation)
+ * @param q3 True attitude quaternion component 3, y (0 in null-rotation)
+ * @param q4 True attitude quaternion component 4, z (0 in null-rotation)
  * @param roll Attitude roll expressed as Euler angles, not recommended except for human-readable outputs
  * @param pitch Attitude pitch expressed as Euler angles, not recommended except for human-readable outputs
  * @param yaw Attitude yaw expressed as Euler angles, not recommended except for human-readable outputs
@@ -161,10 +161,10 @@ static inline uint16_t mavlink_msg_sim_state_pack(uint8_t system_id, uint8_t com
  * @param component_id ID of this component (e.g. 200 for IMU)
  * @param chan The MAVLink channel this message will be sent over
  * @param msg The MAVLink message to compress the data into
- * @param q1 True attitude quaternion component 1
- * @param q2 True attitude quaternion component 2
- * @param q3 True attitude quaternion component 3
- * @param q4 True attitude quaternion component 4
+ * @param q1 True attitude quaternion component 1, w (1 in null-rotation)
+ * @param q2 True attitude quaternion component 2, x (0 in null-rotation)
+ * @param q3 True attitude quaternion component 3, y (0 in null-rotation)
+ * @param q4 True attitude quaternion component 4, z (0 in null-rotation)
  * @param roll Attitude roll expressed as Euler angles, not recommended except for human-readable outputs
  * @param pitch Attitude pitch expressed as Euler angles, not recommended except for human-readable outputs
  * @param yaw Attitude yaw expressed as Euler angles, not recommended except for human-readable outputs
@@ -279,10 +279,10 @@ static inline uint16_t mavlink_msg_sim_state_encode_chan(uint8_t system_id, uint
  * @brief Send a sim_state message
  * @param chan MAVLink channel to send the message
  *
- * @param q1 True attitude quaternion component 1
- * @param q2 True attitude quaternion component 2
- * @param q3 True attitude quaternion component 3
- * @param q4 True attitude quaternion component 4
+ * @param q1 True attitude quaternion component 1, w (1 in null-rotation)
+ * @param q2 True attitude quaternion component 2, x (0 in null-rotation)
+ * @param q3 True attitude quaternion component 3, y (0 in null-rotation)
+ * @param q4 True attitude quaternion component 4, z (0 in null-rotation)
  * @param roll Attitude roll expressed as Euler angles, not recommended except for human-readable outputs
  * @param pitch Attitude pitch expressed as Euler angles, not recommended except for human-readable outputs
  * @param yaw Attitude yaw expressed as Euler angles, not recommended except for human-readable outputs
@@ -446,7 +446,7 @@ static inline void mavlink_msg_sim_state_send_buf(mavlink_message_t *msgbuf, mav
 /**
  * @brief Get field q1 from sim_state message
  *
- * @return True attitude quaternion component 1
+ * @return True attitude quaternion component 1, w (1 in null-rotation)
  */
 static inline float mavlink_msg_sim_state_get_q1(const mavlink_message_t* msg)
 {
@@ -456,7 +456,7 @@ static inline float mavlink_msg_sim_state_get_q1(const mavlink_message_t* msg)
 /**
  * @brief Get field q2 from sim_state message
  *
- * @return True attitude quaternion component 2
+ * @return True attitude quaternion component 2, x (0 in null-rotation)
  */
 static inline float mavlink_msg_sim_state_get_q2(const mavlink_message_t* msg)
 {
@@ -466,7 +466,7 @@ static inline float mavlink_msg_sim_state_get_q2(const mavlink_message_t* msg)
 /**
  * @brief Get field q3 from sim_state message
  *
- * @return True attitude quaternion component 3
+ * @return True attitude quaternion component 3, y (0 in null-rotation)
  */
 static inline float mavlink_msg_sim_state_get_q3(const mavlink_message_t* msg)
 {
@@ -476,7 +476,7 @@ static inline float mavlink_msg_sim_state_get_q3(const mavlink_message_t* msg)
 /**
  * @brief Get field q4 from sim_state message
  *
- * @return True attitude quaternion component 4
+ * @return True attitude quaternion component 4, z (0 in null-rotation)
  */
 static inline float mavlink_msg_sim_state_get_q4(const mavlink_message_t* msg)
 {

common/version.h

@@ -5,7 +5,7 @@
 #ifndef MAVLINK_VERSION_H
 #define MAVLINK_VERSION_H
 
-#define MAVLINK_BUILD_DATE "Thu Jul 24 13:46:04 2014"
+#define MAVLINK_BUILD_DATE "Thu Jul 24 16:11:07 2014"
 #define MAVLINK_WIRE_PROTOCOL_VERSION "1.0"
 #define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
  

matrixpilot/matrixpilot.h

@@ -95,7 +95,7 @@ typedef enum MAV_CMD
 	MAV_CMD_DO_FENCE_ENABLE=207, /* Mission command to enable the geofence |enable? (0=disable, 1=enable)| Empty| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_PARACHUTE=208, /* Mission command to trigger a parachute |action (0=disable, 1=enable, 2=release, for some systems see PARACHUTE_ACTION enum, not in general message set.)| Empty| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_INVERTED_FLIGHT=210, /* Change to/from inverted flight |inverted (0=normal, 1=inverted)| Empty| Empty| Empty| Empty| Empty| Empty|  */
-	MAV_CMD_DO_MOUNT_CONTROL_QUAT=220, /* Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1| q2 - quaternion param #2| q3 - quaternion param #3| q4 - quaternion param #4| Empty| Empty| Empty|  */
+	MAV_CMD_DO_MOUNT_CONTROL_QUAT=220, /* Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1, w (1 in null-rotation)| q2 - quaternion param #2, x (0 in null-rotation)| q3 - quaternion param #3, y (0 in null-rotation)| q4 - quaternion param #4, z (0 in null-rotation)| Empty| Empty| Empty|  */
 	MAV_CMD_DO_GUIDED_MASTER=221, /* set id of master controller |System ID| Component ID| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_GUIDED_LIMITS=222, /* set limits for external control |timeout - maximum time (in seconds) that external controller will be allowed to control vehicle. 0 means no timeout| absolute altitude min (in meters, WGS84) - if vehicle moves below this alt, the command will be aborted and the mission will continue.  0 means no lower altitude limit| absolute altitude max (in meters)- if vehicle moves above this alt, the command will be aborted and the mission will continue.  0 means no upper altitude limit| horizontal move limit (in meters, WGS84) - if vehicle moves more than this distance from it's location at the moment the command was executed, the command will be aborted and the mission will continue. 0 means no horizontal altitude limit| Empty| Empty| Empty|  */
 	MAV_CMD_DO_LAST=240, /* NOP - This command is only used to mark the upper limit of the DO commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty|  */

matrixpilot/version.h

@@ -5,7 +5,7 @@
 #ifndef MAVLINK_VERSION_H
 #define MAVLINK_VERSION_H
 
-#define MAVLINK_BUILD_DATE "Thu Jul 24 13:45:25 2014"
+#define MAVLINK_BUILD_DATE "Thu Jul 24 16:10:27 2014"
 #define MAVLINK_WIRE_PROTOCOL_VERSION "1.0"
 #define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
  

mavlink_conversions.h

@@ -27,6 +27,13 @@
  * @author James Goppert
  */
 
+
+/**
+ * Converts a quaternion to a rotation matrix
+ *
+ * @param quaternion a [w, x, y, z] ordered quaternion (null-rotation being 1 0 0 0)
+ * @param dcm a 3x3 rotation matrix
+ */
 MAVLINK_HELPER void mavlink_quaternion_to_dcm(const float quaternion[4], float dcm[3][3])
 {
     double a = quaternion[0];
@@ -48,6 +55,15 @@ MAVLINK_HELPER void mavlink_quaternion_to_dcm(const float quaternion[4], float d
     dcm[2][2] = aSq - bSq - cSq + dSq;
 }
 
+
+/**
+ * Converts a rotation matrix to euler angles
+ *
+ * @param dcm a 3x3 rotation matrix
+ * @param roll the roll angle in radians
+ * @param pitch the pitch angle in radians
+ * @param yaw the yaw angle in radians
+ */
 MAVLINK_HELPER void mavlink_dcm_to_euler(const float dcm[3][3], float* roll, float* pitch, float* yaw)
 {
     float phi, theta, psi;
@@ -73,6 +89,15 @@ MAVLINK_HELPER void mavlink_dcm_to_euler(const float dcm[3][3], float* roll, flo
     *yaw = psi;
 }
 
+
+/**
+ * Converts a quaternion to euler angles
+ *
+ * @param quaternion a [w, x, y, z] ordered quaternion (null-rotation being 1 0 0 0)
+ * @param roll the roll angle in radians
+ * @param pitch the pitch angle in radians
+ * @param yaw the yaw angle in radians
+ */
 MAVLINK_HELPER void mavlink_quaternion_to_euler(const float quaternion[4], float* roll, float* pitch, float* yaw)
 {
     float dcm[3][3];
@@ -80,6 +105,15 @@ MAVLINK_HELPER void mavlink_quaternion_to_euler(const float quaternion[4], float
     mavlink_dcm_to_euler((const float(*)[3])dcm, roll, pitch, yaw);
 }
 
+
+/**
+ * Converts euler angles to a quaternion
+ *
+ * @param roll the roll angle in radians
+ * @param pitch the pitch angle in radians
+ * @param yaw the yaw angle in radians
+ * @param quaternion a [w, x, y, z] ordered quaternion (null-rotation being 1 0 0 0)
+ */
 MAVLINK_HELPER void mavlink_euler_to_quaternion(float roll, float pitch, float yaw, float quaternion[4])
 {
     double cosPhi_2 = cos((double)roll / 2.0);
@@ -98,6 +132,13 @@ MAVLINK_HELPER void mavlink_euler_to_quaternion(float roll, float pitch, float y
             sinPhi_2 * sinTheta_2 * cosPsi_2);
 }
 
+
+/**
+ * Converts a rotation matrix to a quaternion
+ *
+ * @param dcm a 3x3 rotation matrix
+ * @param quaternion a [w, x, y, z] ordered quaternion (null-rotation being 1 0 0 0)
+ */
 MAVLINK_HELPER void mavlink_dcm_to_quaternion(const float dcm[3][3], float quaternion[4])
 {
     quaternion[0] = (0.5 * sqrt(1.0 +
@@ -110,6 +151,15 @@ MAVLINK_HELPER void mavlink_dcm_to_quaternion(const float dcm[3][3], float quate
             (double)(-dcm[0][0] - dcm[1][1] + dcm[2][2])));
 }
 
+
+/**
+ * Converts euler angles to a rotation matrix
+ *
+ * @param roll the roll angle in radians
+ * @param pitch the pitch angle in radians
+ * @param yaw the yaw angle in radians
+ * @param dcm a 3x3 rotation matrix
+ */
 MAVLINK_HELPER void mavlink_euler_to_dcm(float roll, float pitch, float yaw, float dcm[3][3])
 {
     double cosPhi = cos(roll);

minimal/version.h

@@ -5,7 +5,7 @@
 #ifndef MAVLINK_VERSION_H
 #define MAVLINK_VERSION_H
 
-#define MAVLINK_BUILD_DATE "Thu Jul 24 13:45:32 2014"
+#define MAVLINK_BUILD_DATE "Thu Jul 24 16:10:34 2014"
 #define MAVLINK_WIRE_PROTOCOL_VERSION "1.0"
 #define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 9
  

pixhawk/pixhawk.h

@@ -90,7 +90,7 @@ typedef enum MAV_CMD
 	MAV_CMD_DO_FENCE_ENABLE=207, /* Mission command to enable the geofence |enable? (0=disable, 1=enable)| Empty| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_PARACHUTE=208, /* Mission command to trigger a parachute |action (0=disable, 1=enable, 2=release, for some systems see PARACHUTE_ACTION enum, not in general message set.)| Empty| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_INVERTED_FLIGHT=210, /* Change to/from inverted flight |inverted (0=normal, 1=inverted)| Empty| Empty| Empty| Empty| Empty| Empty|  */
-	MAV_CMD_DO_MOUNT_CONTROL_QUAT=220, /* Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1| q2 - quaternion param #2| q3 - quaternion param #3| q4 - quaternion param #4| Empty| Empty| Empty|  */
+	MAV_CMD_DO_MOUNT_CONTROL_QUAT=220, /* Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1, w (1 in null-rotation)| q2 - quaternion param #2, x (0 in null-rotation)| q3 - quaternion param #3, y (0 in null-rotation)| q4 - quaternion param #4, z (0 in null-rotation)| Empty| Empty| Empty|  */
 	MAV_CMD_DO_GUIDED_MASTER=221, /* set id of master controller |System ID| Component ID| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_GUIDED_LIMITS=222, /* set limits for external control |timeout - maximum time (in seconds) that external controller will be allowed to control vehicle. 0 means no timeout| absolute altitude min (in meters, WGS84) - if vehicle moves below this alt, the command will be aborted and the mission will continue.  0 means no lower altitude limit| absolute altitude max (in meters)- if vehicle moves above this alt, the command will be aborted and the mission will continue.  0 means no upper altitude limit| horizontal move limit (in meters, WGS84) - if vehicle moves more than this distance from it's location at the moment the command was executed, the command will be aborted and the mission will continue. 0 means no horizontal altitude limit| Empty| Empty| Empty|  */
 	MAV_CMD_DO_LAST=240, /* NOP - This command is only used to mark the upper limit of the DO commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty|  */

pixhawk/version.h

@@ -5,7 +5,7 @@
 #ifndef MAVLINK_VERSION_H
 #define MAVLINK_VERSION_H
 
-#define MAVLINK_BUILD_DATE "Thu Jul 24 13:45:33 2014"
+#define MAVLINK_BUILD_DATE "Thu Jul 24 16:10:35 2014"
 #define MAVLINK_WIRE_PROTOCOL_VERSION "1.0"
 #define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
  

sensesoar/version.h

@@ -5,7 +5,7 @@
 #ifndef MAVLINK_VERSION_H
 #define MAVLINK_VERSION_H
 
-#define MAVLINK_BUILD_DATE "Thu Jul 24 13:45:40 2014"
+#define MAVLINK_BUILD_DATE "Thu Jul 24 16:10:42 2014"
 #define MAVLINK_WIRE_PROTOCOL_VERSION "1.0"
 #define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
  

slugs/slugs.h

@@ -78,7 +78,7 @@ typedef enum MAV_CMD
 	MAV_CMD_DO_FENCE_ENABLE=207, /* Mission command to enable the geofence |enable? (0=disable, 1=enable)| Empty| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_PARACHUTE=208, /* Mission command to trigger a parachute |action (0=disable, 1=enable, 2=release, for some systems see PARACHUTE_ACTION enum, not in general message set.)| Empty| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_INVERTED_FLIGHT=210, /* Change to/from inverted flight |inverted (0=normal, 1=inverted)| Empty| Empty| Empty| Empty| Empty| Empty|  */
-	MAV_CMD_DO_MOUNT_CONTROL_QUAT=220, /* Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1| q2 - quaternion param #2| q3 - quaternion param #3| q4 - quaternion param #4| Empty| Empty| Empty|  */
+	MAV_CMD_DO_MOUNT_CONTROL_QUAT=220, /* Mission command to control a camera or antenna mount, using a quaternion as reference. |q1 - quaternion param #1, w (1 in null-rotation)| q2 - quaternion param #2, x (0 in null-rotation)| q3 - quaternion param #3, y (0 in null-rotation)| q4 - quaternion param #4, z (0 in null-rotation)| Empty| Empty| Empty|  */
 	MAV_CMD_DO_GUIDED_MASTER=221, /* set id of master controller |System ID| Component ID| Empty| Empty| Empty| Empty| Empty|  */
 	MAV_CMD_DO_GUIDED_LIMITS=222, /* set limits for external control |timeout - maximum time (in seconds) that external controller will be allowed to control vehicle. 0 means no timeout| absolute altitude min (in meters, WGS84) - if vehicle moves below this alt, the command will be aborted and the mission will continue.  0 means no lower altitude limit| absolute altitude max (in meters)- if vehicle moves above this alt, the command will be aborted and the mission will continue.  0 means no upper altitude limit| horizontal move limit (in meters, WGS84) - if vehicle moves more than this distance from it's location at the moment the command was executed, the command will be aborted and the mission will continue. 0 means no horizontal altitude limit| Empty| Empty| Empty|  */
 	MAV_CMD_DO_LAST=240, /* NOP - This command is only used to mark the upper limit of the DO commands in the enumeration |Empty| Empty| Empty| Empty| Empty| Empty| Empty|  */

slugs/version.h

@@ -5,7 +5,7 @@
 #ifndef MAVLINK_VERSION_H
 #define MAVLINK_VERSION_H
 
-#define MAVLINK_BUILD_DATE "Thu Jul 24 13:45:46 2014"
+#define MAVLINK_BUILD_DATE "Thu Jul 24 16:10:49 2014"
 #define MAVLINK_WIRE_PROTOCOL_VERSION "1.0"
 #define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
  

test/version.h

@@ -5,7 +5,7 @@
 #ifndef MAVLINK_VERSION_H
 #define MAVLINK_VERSION_H
 
-#define MAVLINK_BUILD_DATE "Thu Jul 24 13:45:53 2014"
+#define MAVLINK_BUILD_DATE "Thu Jul 24 16:10:55 2014"
 #define MAVLINK_WIRE_PROTOCOL_VERSION "1.0"
 #define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 179
  

ualberta/version.h

@@ -5,7 +5,7 @@
 #ifndef MAVLINK_VERSION_H
 #define MAVLINK_VERSION_H
 
-#define MAVLINK_BUILD_DATE "Thu Jul 24 13:45:54 2014"
+#define MAVLINK_BUILD_DATE "Thu Jul 24 16:10:56 2014"
 #define MAVLINK_WIRE_PROTOCOL_VERSION "1.0"
 #define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255