@ -653,7 +653,7 @@ Note: ekf2 will limit the delta velocity bias estimate magnitude to be less than
<long_desc>This is the minimum indicated airspeed at which the wing can produce 1g of lift. It is used by the airspeed sensor fault detection and failsafe calculation to detect a significant airspeed low measurement error condition and should be set based on flight test for reliable operation. The failsafe response is controlled by the COM_ASPD_FS_ACT parameter.</long_desc>
<long_desc>This is the minimum indicated airspeed at which the wing can produce 1g of lift. It is used by the airspeed sensor fault detection and failsafe calculation to detect a significant airspeed low measurement error condition and should be set based on flight test for reliable operation. The failsafe response is controlled by the COM_ASPD_FS_ACT parameter.</long_desc>
<short_desc>Time-out for auto disarm after landing</short_desc>
<short_desc>Time-out for auto disarm after landing</short_desc>
<long_desc>A non-zero, positive value specifies the time-out period in seconds after which the vehicle will be automatically disarmed in case a landing situation has been detected during this period. The vehicle will also auto-disarm right after arming if it has not even flown, however the time will always be 10 seconds such that the pilot has enough time to take off. A negative value means that automatic disarming triggered by landing detection is disabled.</long_desc>
<long_desc>A non-zero, positive value specifies the time-out period in seconds after which the vehicle will be automatically disarmed in case a landing situation has been detected during this period. The vehicle will also auto-disarm right after arming if it has not even flown, however the time will always be 10 seconds such that the pilot has enough time to take off. A negative value means that automatic disarming triggered by landing detection is disabled.</long_desc>
PX4BuildBot
6 years ago