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autogenerated headers for rev https://github.com/mavlink/mavlink/tree/a5a4b625fac95c55ad88eb0fcb202321d5f4df96

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PX4BuildBot
2017-04-07 07:21:41 +00:00
parent 53bd663d8e
commit f5581035d0
17 changed files with 45 additions and 45 deletions
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ASLUAV/ASLUAV.h
+5 -5
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@@ -39,13 +39,13 @@ extern "C" {
#define HAVE_ENUM_MAV_CMD
typedef enum MAV_CMD
{
MAV_CMD_NAV_WAYPOINT=16, /* Navigate to MISSION. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)| 0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at MISSION (rotary wing)| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_WAYPOINT=16, /* Navigate to MISSION. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)| 0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at MISSION (rotary wing). NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_UNLIM=17, /* Loiter around this MISSION an unlimited amount of time |Empty| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_TURNS=18, /* Loiter around this MISSION for X turns |Turns| Empty| Radius around MISSION, in meters. 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| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_TIME=19, /* Loiter around this MISSION for X seconds |Seconds (decimal)| Empty| Radius around MISSION, in meters. 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| 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 |Abort Alt| Empty| Empty| Desired yaw angle| Latitude| Longitude| Altitude| */
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| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LAND=21, /* Land at location |Abort Alt| Empty| Empty| Desired yaw angle. NaN for unchanged.| Latitude| Longitude| Altitude| */
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 for unchanged.| 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 [m] - 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 [ms^-1]| Desired yaw angle [rad]| Y-axis position [m]| X-axis position [m]| Z-axis / ground level position [m]| */
MAV_CMD_NAV_TAKEOFF_LOCAL=24, /* Takeoff from local position (local frame only) |Minimum pitch (if airspeed sensor present), desired pitch without sensor [rad]| Empty| Takeoff ascend rate [ms^-1]| Yaw angle [rad] (if magnetometer or another yaw estimation source present), ignored without one of these| Y-axis position [m]| X-axis position [m]| Z-axis position [m]| */
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 MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */
@@ -56,8 +56,8 @@ typedef enum MAV_CMD
MAV_CMD_NAV_ROI=80, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */
MAV_CMD_NAV_PATHPLANNING=81, /* Control autonomous path planning on the MAV. |0: Disable local obstacle avoidance / local path planning (without resetting map), 1: Enable local path planning, 2: Enable and reset local path planning| 0: Disable full path planning (without resetting map), 1: Enable, 2: Enable and reset map/occupancy grid, 3: Enable and reset planned route, but not occupancy grid| Empty| Yaw angle at goal, in compass degrees, [0..360]| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */
MAV_CMD_NAV_SPLINE_WAYPOINT=82, /* Navigate to MISSION using a spline path. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Empty| Empty| Empty| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */
MAV_CMD_NAV_VTOL_TAKEOFF=84, /* Takeoff from ground using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_LAND=85, /* Land using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_TAKEOFF=84, /* Takeoff from ground using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees. NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_LAND=85, /* Land using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees. NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_GUIDED_ENABLE=92, /* hand control over to an external controller |On / Off (> 0.5f on)| Empty| Empty| Empty| Empty| Empty| Empty| */
MAV_CMD_NAV_DELAY=93, /* Delay the next navigation command a number of seconds or until a specified time |Delay in seconds (decimal, -1 to enable time-of-day fields)| hour (24h format, UTC, -1 to ignore)| minute (24h format, UTC, -1 to ignore)| second (24h format, UTC)| Empty| Empty| Empty| */
MAV_CMD_NAV_PAYLOAD_PLACE=94, /* Descend and place payload. Vehicle descends until it detects a hanging payload has reached the ground, the gripper is opened to release the payload |Maximum distance to descend (meters)| Empty| Empty| Empty| Latitude (deg * 1E7)| Longitude (deg * 1E7)| Altitude (meters)| */
ASLUAV/version.h
+1 -1
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@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed Apr 05 2017"
#define MAVLINK_BUILD_DATE "Fri Apr 07 2017"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
ardupilotmega/ardupilotmega.h
+5 -5
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@@ -54,13 +54,13 @@ typedef enum ACCELCAL_VEHICLE_POS
#define HAVE_ENUM_MAV_CMD
typedef enum MAV_CMD
{
MAV_CMD_NAV_WAYPOINT=16, /* Navigate to MISSION. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)| 0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at MISSION (rotary wing)| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_WAYPOINT=16, /* Navigate to MISSION. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)| 0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at MISSION (rotary wing). NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_UNLIM=17, /* Loiter around this MISSION an unlimited amount of time |Empty| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_TURNS=18, /* Loiter around this MISSION for X turns |Turns| Empty| Radius around MISSION, in meters. 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| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_TIME=19, /* Loiter around this MISSION for X seconds |Seconds (decimal)| Empty| Radius around MISSION, in meters. 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| 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 |Abort Alt| Empty| Empty| Desired yaw angle| Latitude| Longitude| Altitude| */
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| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LAND=21, /* Land at location |Abort Alt| Empty| Empty| Desired yaw angle. NaN for unchanged.| Latitude| Longitude| Altitude| */
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 for unchanged.| 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 [m] - 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 [ms^-1]| Desired yaw angle [rad]| Y-axis position [m]| X-axis position [m]| Z-axis / ground level position [m]| */
MAV_CMD_NAV_TAKEOFF_LOCAL=24, /* Takeoff from local position (local frame only) |Minimum pitch (if airspeed sensor present), desired pitch without sensor [rad]| Empty| Takeoff ascend rate [ms^-1]| Yaw angle [rad] (if magnetometer or another yaw estimation source present), ignored without one of these| Y-axis position [m]| X-axis position [m]| Z-axis position [m]| */
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 MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */
@@ -72,8 +72,8 @@ typedef enum MAV_CMD
MAV_CMD_NAV_PATHPLANNING=81, /* Control autonomous path planning on the MAV. |0: Disable local obstacle avoidance / local path planning (without resetting map), 1: Enable local path planning, 2: Enable and reset local path planning| 0: Disable full path planning (without resetting map), 1: Enable, 2: Enable and reset map/occupancy grid, 3: Enable and reset planned route, but not occupancy grid| Empty| Yaw angle at goal, in compass degrees, [0..360]| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */
MAV_CMD_NAV_SPLINE_WAYPOINT=82, /* Navigate to MISSION using a spline path. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Empty| Empty| Empty| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */
MAV_CMD_NAV_ALTITUDE_WAIT=83, /* Mission command to wait for an altitude or downwards vertical speed. This is meant for high altitude balloon launches, allowing the aircraft to be idle until either an altitude is reached or a negative vertical speed is reached (indicating early balloon burst). The wiggle time is how often to wiggle the control surfaces to prevent them seizing up. |altitude (m)| descent speed (m/s)| Wiggle Time (s)| Empty| Empty| Empty| Empty| */
MAV_CMD_NAV_VTOL_TAKEOFF=84, /* Takeoff from ground using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_LAND=85, /* Land using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_TAKEOFF=84, /* Takeoff from ground using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees. NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_LAND=85, /* Land using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees. NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_GUIDED_ENABLE=92, /* hand control over to an external controller |On / Off (> 0.5f on)| Empty| Empty| Empty| Empty| Empty| Empty| */
MAV_CMD_NAV_DELAY=93, /* Delay the next navigation command a number of seconds or until a specified time |Delay in seconds (decimal, -1 to enable time-of-day fields)| hour (24h format, UTC, -1 to ignore)| minute (24h format, UTC, -1 to ignore)| second (24h format, UTC)| Empty| Empty| Empty| */
MAV_CMD_NAV_PAYLOAD_PLACE=94, /* Descend and place payload. Vehicle descends until it detects a hanging payload has reached the ground, the gripper is opened to release the payload |Maximum distance to descend (meters)| Empty| Empty| Empty| Latitude (deg * 1E7)| Longitude (deg * 1E7)| Altitude (meters)| */
ardupilotmega/version.h
+1 -1
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@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed Apr 05 2017"
#define MAVLINK_BUILD_DATE "Fri Apr 07 2017"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
autoquad/autoquad.h
+5 -5
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@@ -83,13 +83,13 @@ typedef enum MAV_CMD
MAV_CMD_AQ_NAV_LEG_ORBIT=1, /* Orbit a waypoint. |Orbit radius in meters| Loiter time in decimal seconds| Maximum horizontal speed in m/s| Desired yaw angle at waypoint| Latitude| Longitude| Altitude| */
MAV_CMD_AQ_TELEMETRY=2, /* Start/stop AutoQuad telemetry values stream. |Start or stop (1 or 0)| Stream frequency in us| Dataset ID (refer to aq_mavlink.h::mavlinkCustomDataSets enum in AQ flight controller code)| Empty| Empty| Empty| Empty| */
MAV_CMD_AQ_REQUEST_VERSION=4, /* Request AutoQuad firmware version number. |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */
MAV_CMD_NAV_WAYPOINT=16, /* Navigate to MISSION. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)| 0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at MISSION (rotary wing)| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_WAYPOINT=16, /* Navigate to MISSION. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)| 0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at MISSION (rotary wing). NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_UNLIM=17, /* Loiter around this MISSION an unlimited amount of time |Empty| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_TURNS=18, /* Loiter around this MISSION for X turns |Turns| Empty| Radius around MISSION, in meters. 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| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_TIME=19, /* Loiter around this MISSION for X seconds |Seconds (decimal)| Empty| Radius around MISSION, in meters. 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| 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 |Abort Alt| Empty| Empty| Desired yaw angle| Latitude| Longitude| Altitude| */
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| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LAND=21, /* Land at location |Abort Alt| Empty| Empty| Desired yaw angle. NaN for unchanged.| Latitude| Longitude| Altitude| */
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 for unchanged.| 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 [m] - 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 [ms^-1]| Desired yaw angle [rad]| Y-axis position [m]| X-axis position [m]| Z-axis / ground level position [m]| */
MAV_CMD_NAV_TAKEOFF_LOCAL=24, /* Takeoff from local position (local frame only) |Minimum pitch (if airspeed sensor present), desired pitch without sensor [rad]| Empty| Takeoff ascend rate [ms^-1]| Yaw angle [rad] (if magnetometer or another yaw estimation source present), ignored without one of these| Y-axis position [m]| X-axis position [m]| Z-axis position [m]| */
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 MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */
@@ -100,8 +100,8 @@ typedef enum MAV_CMD
MAV_CMD_NAV_ROI=80, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */
MAV_CMD_NAV_PATHPLANNING=81, /* Control autonomous path planning on the MAV. |0: Disable local obstacle avoidance / local path planning (without resetting map), 1: Enable local path planning, 2: Enable and reset local path planning| 0: Disable full path planning (without resetting map), 1: Enable, 2: Enable and reset map/occupancy grid, 3: Enable and reset planned route, but not occupancy grid| Empty| Yaw angle at goal, in compass degrees, [0..360]| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */
MAV_CMD_NAV_SPLINE_WAYPOINT=82, /* Navigate to MISSION using a spline path. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Empty| Empty| Empty| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */
MAV_CMD_NAV_VTOL_TAKEOFF=84, /* Takeoff from ground using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_LAND=85, /* Land using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_TAKEOFF=84, /* Takeoff from ground using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees. NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_LAND=85, /* Land using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees. NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_GUIDED_ENABLE=92, /* hand control over to an external controller |On / Off (> 0.5f on)| Empty| Empty| Empty| Empty| Empty| Empty| */
MAV_CMD_NAV_DELAY=93, /* Delay the next navigation command a number of seconds or until a specified time |Delay in seconds (decimal, -1 to enable time-of-day fields)| hour (24h format, UTC, -1 to ignore)| minute (24h format, UTC, -1 to ignore)| second (24h format, UTC)| Empty| Empty| Empty| */
MAV_CMD_NAV_PAYLOAD_PLACE=94, /* Descend and place payload. Vehicle descends until it detects a hanging payload has reached the ground, the gripper is opened to release the payload |Maximum distance to descend (meters)| Empty| Empty| Empty| Latitude (deg * 1E7)| Longitude (deg * 1E7)| Altitude (meters)| */
autoquad/version.h
+1 -1
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@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed Apr 05 2017"
#define MAVLINK_BUILD_DATE "Fri Apr 07 2017"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
common/common.h
+5 -5
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@@ -355,13 +355,13 @@ typedef enum MAV_MOUNT_MODE
#define HAVE_ENUM_MAV_CMD
typedef enum MAV_CMD
{
MAV_CMD_NAV_WAYPOINT=16, /* Navigate to MISSION. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)| 0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at MISSION (rotary wing)| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_WAYPOINT=16, /* Navigate to MISSION. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)| 0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at MISSION (rotary wing). NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_UNLIM=17, /* Loiter around this MISSION an unlimited amount of time |Empty| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_TURNS=18, /* Loiter around this MISSION for X turns |Turns| Empty| Radius around MISSION, in meters. 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| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_TIME=19, /* Loiter around this MISSION for X seconds |Seconds (decimal)| Empty| Radius around MISSION, in meters. 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| 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 |Abort Alt| Empty| Empty| Desired yaw angle| Latitude| Longitude| Altitude| */
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| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LAND=21, /* Land at location |Abort Alt| Empty| Empty| Desired yaw angle. NaN for unchanged.| Latitude| Longitude| Altitude| */
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 for unchanged.| 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 [m] - 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 [ms^-1]| Desired yaw angle [rad]| Y-axis position [m]| X-axis position [m]| Z-axis / ground level position [m]| */
MAV_CMD_NAV_TAKEOFF_LOCAL=24, /* Takeoff from local position (local frame only) |Minimum pitch (if airspeed sensor present), desired pitch without sensor [rad]| Empty| Takeoff ascend rate [ms^-1]| Yaw angle [rad] (if magnetometer or another yaw estimation source present), ignored without one of these| Y-axis position [m]| X-axis position [m]| Z-axis position [m]| */
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 MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */
@@ -372,8 +372,8 @@ typedef enum MAV_CMD
MAV_CMD_NAV_ROI=80, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */
MAV_CMD_NAV_PATHPLANNING=81, /* Control autonomous path planning on the MAV. |0: Disable local obstacle avoidance / local path planning (without resetting map), 1: Enable local path planning, 2: Enable and reset local path planning| 0: Disable full path planning (without resetting map), 1: Enable, 2: Enable and reset map/occupancy grid, 3: Enable and reset planned route, but not occupancy grid| Empty| Yaw angle at goal, in compass degrees, [0..360]| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */
MAV_CMD_NAV_SPLINE_WAYPOINT=82, /* Navigate to MISSION using a spline path. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Empty| Empty| Empty| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */
MAV_CMD_NAV_VTOL_TAKEOFF=84, /* Takeoff from ground using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_LAND=85, /* Land using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_TAKEOFF=84, /* Takeoff from ground using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees. NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_LAND=85, /* Land using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees. NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_GUIDED_ENABLE=92, /* hand control over to an external controller |On / Off (> 0.5f on)| Empty| Empty| Empty| Empty| Empty| Empty| */
MAV_CMD_NAV_DELAY=93, /* Delay the next navigation command a number of seconds or until a specified time |Delay in seconds (decimal, -1 to enable time-of-day fields)| hour (24h format, UTC, -1 to ignore)| minute (24h format, UTC, -1 to ignore)| second (24h format, UTC)| Empty| Empty| Empty| */
MAV_CMD_NAV_PAYLOAD_PLACE=94, /* Descend and place payload. Vehicle descends until it detects a hanging payload has reached the ground, the gripper is opened to release the payload |Maximum distance to descend (meters)| Empty| Empty| Empty| Latitude (deg * 1E7)| Longitude (deg * 1E7)| Altitude (meters)| */
common/version.h
+1 -1
View File
@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed Apr 05 2017"
#define MAVLINK_BUILD_DATE "Fri Apr 07 2017"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
matrixpilot/matrixpilot.h
+5 -5
View File
@@ -56,13 +56,13 @@ typedef enum MAV_PREFLIGHT_STORAGE_ACTION
typedef enum MAV_CMD
{
MAV_CMD_PREFLIGHT_STORAGE_ADVANCED=0, /* Request storage of different parameter values and logs. This command will be only accepted if in pre-flight mode. |Storage action: Action defined by MAV_PREFLIGHT_STORAGE_ACTION_ADVANCED| Storage area as defined by parameter database| Storage flags as defined by parameter database| Empty| Empty| Empty| Empty| */
MAV_CMD_NAV_WAYPOINT=16, /* Navigate to MISSION. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)| 0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at MISSION (rotary wing)| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_WAYPOINT=16, /* Navigate to MISSION. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)| 0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at MISSION (rotary wing). NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_UNLIM=17, /* Loiter around this MISSION an unlimited amount of time |Empty| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_TURNS=18, /* Loiter around this MISSION for X turns |Turns| Empty| Radius around MISSION, in meters. 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| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_TIME=19, /* Loiter around this MISSION for X seconds |Seconds (decimal)| Empty| Radius around MISSION, in meters. 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| 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 |Abort Alt| Empty| Empty| Desired yaw angle| Latitude| Longitude| Altitude| */
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| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LAND=21, /* Land at location |Abort Alt| Empty| Empty| Desired yaw angle. NaN for unchanged.| Latitude| Longitude| Altitude| */
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 for unchanged.| 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 [m] - 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 [ms^-1]| Desired yaw angle [rad]| Y-axis position [m]| X-axis position [m]| Z-axis / ground level position [m]| */
MAV_CMD_NAV_TAKEOFF_LOCAL=24, /* Takeoff from local position (local frame only) |Minimum pitch (if airspeed sensor present), desired pitch without sensor [rad]| Empty| Takeoff ascend rate [ms^-1]| Yaw angle [rad] (if magnetometer or another yaw estimation source present), ignored without one of these| Y-axis position [m]| X-axis position [m]| Z-axis position [m]| */
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 MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */
@@ -73,8 +73,8 @@ typedef enum MAV_CMD
MAV_CMD_NAV_ROI=80, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */
MAV_CMD_NAV_PATHPLANNING=81, /* Control autonomous path planning on the MAV. |0: Disable local obstacle avoidance / local path planning (without resetting map), 1: Enable local path planning, 2: Enable and reset local path planning| 0: Disable full path planning (without resetting map), 1: Enable, 2: Enable and reset map/occupancy grid, 3: Enable and reset planned route, but not occupancy grid| Empty| Yaw angle at goal, in compass degrees, [0..360]| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */
MAV_CMD_NAV_SPLINE_WAYPOINT=82, /* Navigate to MISSION using a spline path. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Empty| Empty| Empty| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */
MAV_CMD_NAV_VTOL_TAKEOFF=84, /* Takeoff from ground using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_LAND=85, /* Land using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_TAKEOFF=84, /* Takeoff from ground using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees. NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_LAND=85, /* Land using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees. NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_GUIDED_ENABLE=92, /* hand control over to an external controller |On / Off (> 0.5f on)| Empty| Empty| Empty| Empty| Empty| Empty| */
MAV_CMD_NAV_DELAY=93, /* Delay the next navigation command a number of seconds or until a specified time |Delay in seconds (decimal, -1 to enable time-of-day fields)| hour (24h format, UTC, -1 to ignore)| minute (24h format, UTC, -1 to ignore)| second (24h format, UTC)| Empty| Empty| Empty| */
MAV_CMD_NAV_PAYLOAD_PLACE=94, /* Descend and place payload. Vehicle descends until it detects a hanging payload has reached the ground, the gripper is opened to release the payload |Maximum distance to descend (meters)| Empty| Empty| Empty| Latitude (deg * 1E7)| Longitude (deg * 1E7)| Altitude (meters)| */
matrixpilot/version.h
+1 -1
View File
@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed Apr 05 2017"
#define MAVLINK_BUILD_DATE "Fri Apr 07 2017"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
message_definitions/common.xml
+5 -5
View File
@@ -593,7 +593,7 @@
<param index="1">Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)</param>
<param index="2">Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)</param>
<param index="3">0 to pass through the WP, if &gt; 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.</param>
<param index="4">Desired yaw angle at MISSION (rotary wing)</param>
<param index="4">Desired yaw angle at MISSION (rotary wing). NaN for unchanged.</param>
<param index="5">Latitude</param>
<param index="6">Longitude</param>
<param index="7">Altitude</param>
@@ -643,7 +643,7 @@
<param index="1">Abort Alt</param>
<param index="2">Empty</param>
<param index="3">Empty</param>
<param index="4">Desired yaw angle</param>
<param index="4">Desired yaw angle. NaN for unchanged.</param>
<param index="5">Latitude</param>
<param index="6">Longitude</param>
<param index="7">Altitude</param>
@@ -653,7 +653,7 @@
<param index="1">Minimum pitch (if airspeed sensor present), desired pitch without sensor</param>
<param index="2">Empty</param>
<param index="3">Empty</param>
<param index="4">Yaw angle (if magnetometer present), ignored without magnetometer</param>
<param index="4">Yaw angle (if magnetometer present), ignored without magnetometer. NaN for unchanged.</param>
<param index="5">Latitude</param>
<param index="6">Longitude</param>
<param index="7">Altitude</param>
@@ -763,7 +763,7 @@
<param index="1">Empty</param>
<param index="2">Empty</param>
<param index="3">Empty</param>
<param index="4">Yaw angle in degrees</param>
<param index="4">Yaw angle in degrees. NaN for unchanged.</param>
<param index="5">Latitude</param>
<param index="6">Longitude</param>
<param index="7">Altitude</param>
@@ -773,7 +773,7 @@
<param index="1">Empty</param>
<param index="2">Empty</param>
<param index="3">Empty</param>
<param index="4">Yaw angle in degrees</param>
<param index="4">Yaw angle in degrees. NaN for unchanged.</param>
<param index="5">Latitude</param>
<param index="6">Longitude</param>
<param index="7">Altitude</param>
minimal/version.h
+1 -1
View File
@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed Apr 05 2017"
#define MAVLINK_BUILD_DATE "Fri Apr 07 2017"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 9
slugs/slugs.h
+5 -5
View File
@@ -39,13 +39,13 @@ extern "C" {
#define HAVE_ENUM_MAV_CMD
typedef enum MAV_CMD
{
MAV_CMD_NAV_WAYPOINT=16, /* Navigate to MISSION. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)| 0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at MISSION (rotary wing)| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_WAYPOINT=16, /* Navigate to MISSION. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Acceptance radius in meters (if the sphere with this radius is hit, the MISSION counts as reached)| 0 to pass through the WP, if > 0 radius in meters to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at MISSION (rotary wing). NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_UNLIM=17, /* Loiter around this MISSION an unlimited amount of time |Empty| Empty| Radius around MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_TURNS=18, /* Loiter around this MISSION for X turns |Turns| Empty| Radius around MISSION, in meters. 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| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LOITER_TIME=19, /* Loiter around this MISSION for X seconds |Seconds (decimal)| Empty| Radius around MISSION, in meters. 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| 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 |Abort Alt| Empty| Empty| Desired yaw angle| Latitude| Longitude| Altitude| */
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| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_LAND=21, /* Land at location |Abort Alt| Empty| Empty| Desired yaw angle. NaN for unchanged.| Latitude| Longitude| Altitude| */
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 for unchanged.| 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 [m] - 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 [ms^-1]| Desired yaw angle [rad]| Y-axis position [m]| X-axis position [m]| Z-axis / ground level position [m]| */
MAV_CMD_NAV_TAKEOFF_LOCAL=24, /* Takeoff from local position (local frame only) |Minimum pitch (if airspeed sensor present), desired pitch without sensor [rad]| Empty| Takeoff ascend rate [ms^-1]| Yaw angle [rad] (if magnetometer or another yaw estimation source present), ignored without one of these| Y-axis position [m]| X-axis position [m]| Z-axis position [m]| */
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 MISSION, in meters. If positive loiter clockwise, else counter-clockwise| Desired yaw angle.| Latitude| Longitude| Altitude| */
@@ -56,8 +56,8 @@ typedef enum MAV_CMD
MAV_CMD_NAV_ROI=80, /* Sets the region of interest (ROI) for a sensor set or the vehicle itself. This can then be used by the vehicles control system to control the vehicle attitude and the attitude of various sensors such as cameras. |Region of intereset mode. (see MAV_ROI enum)| MISSION index/ target ID. (see MAV_ROI enum)| ROI index (allows a vehicle to manage multiple ROI's)| Empty| x the location of the fixed ROI (see MAV_FRAME)| y| z| */
MAV_CMD_NAV_PATHPLANNING=81, /* Control autonomous path planning on the MAV. |0: Disable local obstacle avoidance / local path planning (without resetting map), 1: Enable local path planning, 2: Enable and reset local path planning| 0: Disable full path planning (without resetting map), 1: Enable, 2: Enable and reset map/occupancy grid, 3: Enable and reset planned route, but not occupancy grid| Empty| Yaw angle at goal, in compass degrees, [0..360]| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */
MAV_CMD_NAV_SPLINE_WAYPOINT=82, /* Navigate to MISSION using a spline path. |Hold time in decimal seconds. (ignored by fixed wing, time to stay at MISSION for rotary wing)| Empty| Empty| Empty| Latitude/X of goal| Longitude/Y of goal| Altitude/Z of goal| */
MAV_CMD_NAV_VTOL_TAKEOFF=84, /* Takeoff from ground using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_LAND=85, /* Land using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_TAKEOFF=84, /* Takeoff from ground using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees. NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_VTOL_LAND=85, /* Land using VTOL mode |Empty| Empty| Empty| Yaw angle in degrees. NaN for unchanged.| Latitude| Longitude| Altitude| */
MAV_CMD_NAV_GUIDED_ENABLE=92, /* hand control over to an external controller |On / Off (> 0.5f on)| Empty| Empty| Empty| Empty| Empty| Empty| */
MAV_CMD_NAV_DELAY=93, /* Delay the next navigation command a number of seconds or until a specified time |Delay in seconds (decimal, -1 to enable time-of-day fields)| hour (24h format, UTC, -1 to ignore)| minute (24h format, UTC, -1 to ignore)| second (24h format, UTC)| Empty| Empty| Empty| */
MAV_CMD_NAV_PAYLOAD_PLACE=94, /* Descend and place payload. Vehicle descends until it detects a hanging payload has reached the ground, the gripper is opened to release the payload |Maximum distance to descend (meters)| Empty| Empty| Empty| Latitude (deg * 1E7)| Longitude (deg * 1E7)| Altitude (meters)| */
slugs/version.h
+1 -1
View File
@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed Apr 05 2017"
#define MAVLINK_BUILD_DATE "Fri Apr 07 2017"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
standard/version.h
+1 -1
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@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed Apr 05 2017"
#define MAVLINK_BUILD_DATE "Fri Apr 07 2017"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255
test/version.h
+1 -1
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@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed Apr 05 2017"
#define MAVLINK_BUILD_DATE "Fri Apr 07 2017"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 179
uAvionix/version.h
+1 -1
View File
@@ -7,7 +7,7 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Wed Apr 05 2017"
#define MAVLINK_BUILD_DATE "Fri Apr 07 2017"
#define MAVLINK_WIRE_PROTOCOL_VERSION "2.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 255