摘要 |
<p>Embodiments are directed to causing, by a computing device comprising a processor, a rotating tail rotor to operate in a tail rotor mode when an aircraft is operating at a speed less than a rudder control power threshold, receiving, by the computing device, a command that indicates a request to transition the aircraft, determining, by the computing device, that a rudder of the aircraft has control power in an amount greater than a second threshold based on receiving the command, and causing, by the computing device, the rotating tail rotor to operate in a pusher propeller mode based on determining that the rudder has control power in the amount greater than the second threshold.</p> |
申请人 |
SIKORSKY AIRCRAFT CORPORATION |
发明人 |
LITWINOWICZ, ANTHONY;RIGSBY, JAMES;FEGELY, CODY;SCOTT, MARK W.;KNAG, JOHN |