Invention Grant
US08851419B2 Method and apparatus for changing a deployed position for a tail skid assembly 有权
用于改变尾部滑行组件的展开位置的方法和装置

Method and apparatus for changing a deployed position for a tail skid assembly
Abstract:
A method and apparatus for positioning a tail skid assembly for a maximum rotation angle for an aircraft may be provided. A determination may be made as to whether the tail skid assembly is to be deployed for takeoff or landing. A set of parameters may be identified based on a determination of whether the tail skid assembly is to be deployed for takeoff or landing. A desired maximum rotation angle for the aircraft may be identified using the set of parameters. The tail skid assembly may be deployed to allow the desired maximum rotation angle for the aircraft.
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