mavlink库转换的源码

/* AUTO-GENERATED FILE. DO NOT MODIFY. * * This class was automatically generated by the * java mavlink generator tool. It should not be modified by hand. */ package com.MAVLink.enums; /** * Commands to be executed by the MAV. They can be executed on user request, or as part of a mission script. If the action is used in a mission, the parameter mapping to the waypoint/mission message is as follows: Param 1, Param 2, Param 3, Param 4, X: Param 5, Y:Param 6, Z:Param 7. This command list is similar what ARINC 424 is for commercial aircraft: A data format how to interpret waypoint/mission data. NaN and INT32_MAX may be used in float/integer params (respectively) to indicate optional/default values (e.g. to use the component's current yaw or latitude rather than a specific value). See https://mavlink.io/en/guide/xml_schema.html#MAV_CMD for information about the structure of the MAV_CMD entries */ public class MAV_CMD { public static final int MAV_CMD_NAV_WAYPOINT = 16; /* Navigate to waypoint. |Hold time. (ignored by fixed wing, time to stay at waypoint for rotary wing)| Acceptance radius (if the sphere with this radius is hit, the waypoint counts as reached)| 0 to pass through the WP, if > 0 radius to pass by WP. Positive value for clockwise orbit, negative value for counter-clockwise orbit. Allows trajectory control.| Desired yaw angle at waypoint (rotary wing). NaN to use the current system yaw heading mode (e.g. yaw towards next waypoint, yaw to home, etc.).| Latitude| Longitude| Altitude| */ public static final int MAV_CMD_NAV_LOITER_UNLIM = 17; /* Loiter around this waypoint an unlimited amount of time |Empty| Empty| Loiter radius around waypoint for forward-only moving vehicles (not multicopters). If positive loiter clockwise, else counter-clockwise| 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| */ public static final int MAV_CMD_NAV_LOITER_TURNS = 18; /* Loiter around this waypoint for X turns |Number of turns.| Leave loiter circle only once heading towards the next waypoint (0 = False)| Loiter radius around waypoint for forward-only moving vehicles (not multicopters). If positive loiter clockwise, else counter-clockwise| Loiter circle exit location and/or path to next waypoint ("xtrack") for forward-only moving vehicles (not multicopters). 0 for the vehicle to converge towards the center xtrack when it leaves the loiter (the line between the centers of the current and next waypoint), 1 to converge to the direct line between the location that the vehicle exits the loiter radius and the next waypoint. Otherwise the angle (in degrees) between the tangent of the loiter circle and the center xtrack at which the vehicle must leave the loiter (and converge to the center xtrack). NaN to use the current system default xtrack behaviour.| Latitude| Longitude| Altitude| */ public static final int MAV_CMD_NAV_LOITER_TIME = 19; /* Loiter at the specified latitude, longitude and altitude for a certain amount of time. Multicopter vehicles stop at the point (within a vehicle-specific acceptance radius). Forward-only moving vehicles (e.g. fixed-wing) circle the point with the specified radius/direction. If the Heading Required parameter (2) is non-zero forward moving aircraft will only leave the loiter circle once heading towards the next waypoint. |Loiter time (only starts once Lat, Lon and Alt is reached).| Leave loiter circle only once heading towards the next waypoint (0 = False)| Loiter radius around waypoint for forward-only moving vehicles (not multicopters). If positive loiter clockwise, else counter-clockwise.| Loiter circle exit location and/or path to next waypoint ("xtrack") for forward-only moving vehicles (not multicopters). 0 for the vehicle to converge towards the center xtrack when it leaves the loiter (the line between the centers of the current and next waypoint), 1 to converge to the direct line between the location that the vehicle exits the loiter radius and the next waypoint. Otherwise the angle (in degrees) between the tangent of the loiter circle and the center xtrack at which the vehicle must leave the loiter (and converge to the center xtrack). NaN to use the current system default xtrack behaviour.| Latitude| Longitude| Altitude| */ public static final int MAV_CMD_NAV_RETURN_TO_LAUNCH = 20; /* Return to launch location |Empty| Empty| Empty| Empty| Empty| Empty| Empty| */ public static final int 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).| */ public static final int 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| */ public static final int 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| */ public static final int 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| */ public static final int 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| */ public static final int MAV_CMD_NAV_CONTINUE_AND_CHANGE_ALT = 30; /* Continue on the current course and climb/descend to specified altitude. When the altitude is reached continue to the next command (i.e., don't proceed to the next command until the desired altitude is reached. |Climb or Descend (0 = Neutral, command completes when within 5m of this command's altitude, 1 = Climbing, command completes when at or above this command's altitude, 2 = Descending, command completes when at or below this command's altitude.| Empty| Empty| Empty| Empty| Empty| Desired altitude| */ public static final int MAV_CMD_NAV_LOITER_TO_ALT = 31; /* Begin loiter at the specified Latitude and Longitude. If Lat=Lon=0, then loiter at the current position. Don't consider the navigation command complete (don't leave loiter) until the altitude has been reached. Additionally, if the Heading Required parameter is non-zero the aircraft will not leave the loiter until heading toward the next waypoint. |Leave loiter circle only once heading towards the next waypoint (0 = False)| Loiter radius around waypoint for forward-only moving vehicles (not multicopters). If positive loiter clockwise, negative counter-clockwise, 0 means no change to standard loiter.| Empty| Loiter circle exit location and/o