autogenerated headers for rev...

autogenerated headers for rev https://github.com/mavlink/mavlink/tree/ddc09ce654f0923f3780a7422e14aa0d643f8a80

ASLUAV/ASLUAV.h

@@ -45,7 +45,7 @@ typedef enum MAV_CMD
    MAV_CMD_NAV_LOITER_TIME=19, /* Loiter around this waypoint for X seconds |Loiter time.| Empty| Radius around waypoint. If positive loiter clockwise, else counter-clockwise.| Forward moving aircraft this sets exit xtrack location: 0 for center of loiter wp, 1 for exit location. Else, this is desired yaw angle.  NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
    MAV_CMD_NAV_RETURN_TO_LAUNCH=20, /* Return to launch location |Empty| Empty| Empty| Empty| Empty| Empty| Empty|  */
    MAV_CMD_NAV_LAND=21, /* Land at location. |Minimum target altitude if landing is aborted (0 = undefined/use system default).| Precision land mode.| Empty.| Desired yaw angle. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude.| Longitude.| Landing altitude (ground level in current frame).|  */
-   MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
+   MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand. Vehicles that support multiple takeoff modes (e.g. VTOL quadplane) should take off using the currently configured mode. |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
    MAV_CMD_NAV_LAND_LOCAL=23, /* Land at local position (local frame only) |Landing target number (if available)| Maximum accepted offset from desired landing position - computed magnitude from spherical coordinates: d = sqrt(x^2 + y^2 + z^2), which gives the maximum accepted distance between the desired landing position and the position where the vehicle is about to land| Landing descend rate| Desired yaw angle| Y-axis position| X-axis position| Z-axis / ground level position|  */
    MAV_CMD_NAV_TAKEOFF_LOCAL=24, /* Takeoff from local position (local frame only) |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Takeoff ascend rate| Yaw angle (if magnetometer or another yaw estimation source present), ignored without one of these| Y-axis position| X-axis position| Z-axis position|  */
    MAV_CMD_NAV_FOLLOW=25, /* Vehicle following, i.e. this waypoint represents the position of a moving vehicle |Following logic to use (e.g. loitering or sinusoidal following) - depends on specific autopilot implementation| Ground speed of vehicle to be followed| Radius around waypoint. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude|  */

ardupilotmega/ardupilotmega.h

@@ -62,7 +62,7 @@ typedef enum MAV_CMD
    MAV_CMD_NAV_LOITER_TIME=19, /* Loiter around this waypoint for X seconds |Loiter time.| Empty| Radius around waypoint. If positive loiter clockwise, else counter-clockwise.| Forward moving aircraft this sets exit xtrack location: 0 for center of loiter wp, 1 for exit location. Else, this is desired yaw angle.  NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
    MAV_CMD_NAV_RETURN_TO_LAUNCH=20, /* Return to launch location |Empty| Empty| Empty| Empty| Empty| Empty| Empty|  */
    MAV_CMD_NAV_LAND=21, /* Land at location. |Minimum target altitude if landing is aborted (0 = undefined/use system default).| Precision land mode.| Empty.| Desired yaw angle. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude.| Longitude.| Landing altitude (ground level in current frame).|  */
-   MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
+   MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand. Vehicles that support multiple takeoff modes (e.g. VTOL quadplane) should take off using the currently configured mode. |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
    MAV_CMD_NAV_LAND_LOCAL=23, /* Land at local position (local frame only) |Landing target number (if available)| Maximum accepted offset from desired landing position - computed magnitude from spherical coordinates: d = sqrt(x^2 + y^2 + z^2), which gives the maximum accepted distance between the desired landing position and the position where the vehicle is about to land| Landing descend rate| Desired yaw angle| Y-axis position| X-axis position| Z-axis / ground level position|  */
    MAV_CMD_NAV_TAKEOFF_LOCAL=24, /* Takeoff from local position (local frame only) |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Takeoff ascend rate| Yaw angle (if magnetometer or another yaw estimation source present), ignored without one of these| Y-axis position| X-axis position| Z-axis position|  */
    MAV_CMD_NAV_FOLLOW=25, /* Vehicle following, i.e. this waypoint represents the position of a moving vehicle |Following logic to use (e.g. loitering or sinusoidal following) - depends on specific autopilot implementation| Ground speed of vehicle to be followed| Radius around waypoint. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude|  */

autoquad/autoquad.h

@@ -89,7 +89,7 @@ typedef enum MAV_CMD
    MAV_CMD_NAV_LOITER_TIME=19, /* Loiter around this waypoint for X seconds |Loiter time.| Empty| Radius around waypoint. If positive loiter clockwise, else counter-clockwise.| Forward moving aircraft this sets exit xtrack location: 0 for center of loiter wp, 1 for exit location. Else, this is desired yaw angle.  NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
    MAV_CMD_NAV_RETURN_TO_LAUNCH=20, /* Return to launch location |Empty| Empty| Empty| Empty| Empty| Empty| Empty|  */
    MAV_CMD_NAV_LAND=21, /* Land at location. |Minimum target altitude if landing is aborted (0 = undefined/use system default).| Precision land mode.| Empty.| Desired yaw angle. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude.| Longitude.| Landing altitude (ground level in current frame).|  */
-   MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
+   MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand. Vehicles that support multiple takeoff modes (e.g. VTOL quadplane) should take off using the currently configured mode. |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
    MAV_CMD_NAV_LAND_LOCAL=23, /* Land at local position (local frame only) |Landing target number (if available)| Maximum accepted offset from desired landing position - computed magnitude from spherical coordinates: d = sqrt(x^2 + y^2 + z^2), which gives the maximum accepted distance between the desired landing position and the position where the vehicle is about to land| Landing descend rate| Desired yaw angle| Y-axis position| X-axis position| Z-axis / ground level position|  */
    MAV_CMD_NAV_TAKEOFF_LOCAL=24, /* Takeoff from local position (local frame only) |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Takeoff ascend rate| Yaw angle (if magnetometer or another yaw estimation source present), ignored without one of these| Y-axis position| X-axis position| Z-axis position|  */
    MAV_CMD_NAV_FOLLOW=25, /* Vehicle following, i.e. this waypoint represents the position of a moving vehicle |Following logic to use (e.g. loitering or sinusoidal following) - depends on specific autopilot implementation| Ground speed of vehicle to be followed| Radius around waypoint. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude|  */

common/common.h

@@ -692,7 +692,7 @@ typedef enum MAV_CMD
    MAV_CMD_NAV_LOITER_TIME=19, /* Loiter around this waypoint for X seconds |Loiter time.| Empty| Radius around waypoint. If positive loiter clockwise, else counter-clockwise.| Forward moving aircraft this sets exit xtrack location: 0 for center of loiter wp, 1 for exit location. Else, this is desired yaw angle.  NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
    MAV_CMD_NAV_RETURN_TO_LAUNCH=20, /* Return to launch location |Empty| Empty| Empty| Empty| Empty| Empty| Empty|  */
    MAV_CMD_NAV_LAND=21, /* Land at location. |Minimum target altitude if landing is aborted (0 = undefined/use system default).| Precision land mode.| Empty.| Desired yaw angle. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude.| Longitude.| Landing altitude (ground level in current frame).|  */
-   MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
+   MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand. Vehicles that support multiple takeoff modes (e.g. VTOL quadplane) should take off using the currently configured mode. |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
    MAV_CMD_NAV_LAND_LOCAL=23, /* Land at local position (local frame only) |Landing target number (if available)| Maximum accepted offset from desired landing position - computed magnitude from spherical coordinates: d = sqrt(x^2 + y^2 + z^2), which gives the maximum accepted distance between the desired landing position and the position where the vehicle is about to land| Landing descend rate| Desired yaw angle| Y-axis position| X-axis position| Z-axis / ground level position|  */
    MAV_CMD_NAV_TAKEOFF_LOCAL=24, /* Takeoff from local position (local frame only) |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Takeoff ascend rate| Yaw angle (if magnetometer or another yaw estimation source present), ignored without one of these| Y-axis position| X-axis position| Z-axis position|  */
    MAV_CMD_NAV_FOLLOW=25, /* Vehicle following, i.e. this waypoint represents the position of a moving vehicle |Following logic to use (e.g. loitering or sinusoidal following) - depends on specific autopilot implementation| Ground speed of vehicle to be followed| Radius around waypoint. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude|  */

matrixpilot/matrixpilot.h

@@ -62,7 +62,7 @@ typedef enum MAV_CMD
    MAV_CMD_NAV_LOITER_TIME=19, /* Loiter around this waypoint for X seconds |Loiter time.| Empty| Radius around waypoint. If positive loiter clockwise, else counter-clockwise.| Forward moving aircraft this sets exit xtrack location: 0 for center of loiter wp, 1 for exit location. Else, this is desired yaw angle.  NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
    MAV_CMD_NAV_RETURN_TO_LAUNCH=20, /* Return to launch location |Empty| Empty| Empty| Empty| Empty| Empty| Empty|  */
    MAV_CMD_NAV_LAND=21, /* Land at location. |Minimum target altitude if landing is aborted (0 = undefined/use system default).| Precision land mode.| Empty.| Desired yaw angle. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude.| Longitude.| Landing altitude (ground level in current frame).|  */
-   MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
+   MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand. Vehicles that support multiple takeoff modes (e.g. VTOL quadplane) should take off using the currently configured mode. |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
    MAV_CMD_NAV_LAND_LOCAL=23, /* Land at local position (local frame only) |Landing target number (if available)| Maximum accepted offset from desired landing position - computed magnitude from spherical coordinates: d = sqrt(x^2 + y^2 + z^2), which gives the maximum accepted distance between the desired landing position and the position where the vehicle is about to land| Landing descend rate| Desired yaw angle| Y-axis position| X-axis position| Z-axis / ground level position|  */
    MAV_CMD_NAV_TAKEOFF_LOCAL=24, /* Takeoff from local position (local frame only) |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Takeoff ascend rate| Yaw angle (if magnetometer or another yaw estimation source present), ignored without one of these| Y-axis position| X-axis position| Z-axis position|  */
    MAV_CMD_NAV_FOLLOW=25, /* Vehicle following, i.e. this waypoint represents the position of a moving vehicle |Following logic to use (e.g. loitering or sinusoidal following) - depends on specific autopilot implementation| Ground speed of vehicle to be followed| Radius around waypoint. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude|  */

message_definitions/common.xml

@@ -1348,7 +1348,7 @@
         <param index="7" label="Altitude" units="m">Landing altitude (ground level in current frame).</param>
       </entry>
       <entry value="22" name="MAV_CMD_NAV_TAKEOFF" hasLocation="true" isDestination="true">
-        <description>Takeoff from ground / hand</description>
+        <description>Takeoff from ground / hand. Vehicles that support multiple takeoff modes (e.g. VTOL quadplane) should take off using the currently configured mode.</description>
         <param index="1" label="Pitch">Minimum pitch (if airspeed sensor present), desired pitch without sensor</param>
         <param index="2">Empty</param>
         <param index="3">Empty</param>

slugs/slugs.h

@@ -45,7 +45,7 @@ typedef enum MAV_CMD
    MAV_CMD_NAV_LOITER_TIME=19, /* Loiter around this waypoint for X seconds |Loiter time.| Empty| Radius around waypoint. If positive loiter clockwise, else counter-clockwise.| Forward moving aircraft this sets exit xtrack location: 0 for center of loiter wp, 1 for exit location. Else, this is desired yaw angle.  NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
    MAV_CMD_NAV_RETURN_TO_LAUNCH=20, /* Return to launch location |Empty| Empty| Empty| Empty| Empty| Empty| Empty|  */
    MAV_CMD_NAV_LAND=21, /* Land at location. |Minimum target altitude if landing is aborted (0 = undefined/use system default).| Precision land mode.| Empty.| Desired yaw angle. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude.| Longitude.| Landing altitude (ground level in current frame).|  */
-   MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
+   MAV_CMD_NAV_TAKEOFF=22, /* Takeoff from ground / hand. Vehicles that support multiple takeoff modes (e.g. VTOL quadplane) should take off using the currently configured mode. |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Empty| Yaw angle (if magnetometer present), ignored without magnetometer. NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude|  */
    MAV_CMD_NAV_LAND_LOCAL=23, /* Land at local position (local frame only) |Landing target number (if available)| Maximum accepted offset from desired landing position - computed magnitude from spherical coordinates: d = sqrt(x^2 + y^2 + z^2), which gives the maximum accepted distance between the desired landing position and the position where the vehicle is about to land| Landing descend rate| Desired yaw angle| Y-axis position| X-axis position| Z-axis / ground level position|  */
    MAV_CMD_NAV_TAKEOFF_LOCAL=24, /* Takeoff from local position (local frame only) |Minimum pitch (if airspeed sensor present), desired pitch without sensor| Empty| Takeoff ascend rate| Yaw angle (if magnetometer or another yaw estimation source present), ignored without one of these| Y-axis position| X-axis position| Z-axis position|  */
    MAV_CMD_NAV_FOLLOW=25, /* Vehicle following, i.e. this waypoint represents the position of a moving vehicle |Following logic to use (e.g. loitering or sinusoidal following) - depends on specific autopilot implementation| Ground speed of vehicle to be followed| Radius around waypoint. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude|  */