<short_desc>Integer bitmask controlling handling of magnetic declination. Set bits to in the following positions to enable functions.
0 : Set to true to use the declination from the geo_lookup library when the GPS position becomes available, set to false to always use the EKF2_MAG_DECL value.
1 : Set to true to save the EKF2_MAG_DECL parameter to the value returned by the EKF when the vehicle disarms.
2 : Set to true to always use the declination as an observaton when 3-axis magnetometer fusion is being used</short_desc>
<long_desc>This is the minimum throttle while on the ground For aircraft with internal combustion engine this parameter should be set above desired idle rpm.</long_desc>
<long_desc>Delay between starting attitude control and powering up the throttle (giving throttle control to the controller) Before this timespan is up the throttle will be set to LAUN_THR_PRE, set to 0 to deactivate</long_desc>
<long_desc>Delay between starting attitude control and powering up the throttle (giving throttle control to the controller) Before this timespan is up the throttle will be set to FW_THR_IDLE, set to 0 to deactivate</long_desc>
<short_desc>Time in seconds we wait on reaching target heading at a waypoint if it is forced</short_desc>
<long_desc>If set > 0 it will ignore the target heading for normal waypoint acceptance. If the waypoint forces the heading the timeout will matter. For example on VTOL forwards transiton. Mainly useful for VTOLs that have less yaw authority and might not reach target yaw in wind. Disabled by default.</long_desc>
<long_desc>Vertical thrust required to hover. This value is mapped to center stick for manual throttle control. With this value set to the thrust required to hover, transition from manual to ALTCTL mode while hovering will occur with the throttle stick near center, which is then interpreted as (near) zero demand for vertical speed.</long_desc>
<long_desc>Halfwidth of deadband or reduced sensitivity center portion of curve. This is the halfwidth of the center region of the ALTCTL throttle curve. It extends from center-dz to center+dz.</long_desc>
<long_desc>Controls the slope of the reduced sensitivity region. This is the height of the ALTCTL throttle curve at center-dz and center+dz.</long_desc>
<short_desc>Maximum thrust in auto thrust control</short_desc>
<long_desc>Limit max allowed thrust. Setting a value of one can put the system into actuator saturation as no spread between the motors is possible any more. A value of 0.8 - 0.9 is recommended.</long_desc>
<long_desc>the difference in hours and minutes from Coordinated Universal Time (UTC) for a your place and date. for example, In case of South Korea(UTC+09:00), UTC offset is 540 min (9*60) refer to https://en.wikipedia.org/wiki/List_of_UTC_time_offsets</long_desc>
