发明名称 Pilot Assistance System
摘要 According to one embodiment, a pilot assistance system includes a trim assembly and a trim assembly control system. The trim assembly is operable to communicate with a pilot control device and operable to apply a force against the pilot control device in resistance of a command received from a pilot via the pilot control device. The trim assembly control system is in communication with the trim assembly, configured to identify a first pilot control device position relative to a reference pilot control device position, and configured to instruct the trim assembly to apply a cueing force against the pilot control device if the pilot control device is positioned proximate to the first pilot control device position.
申请公布号 US2017017241(A1) 申请公布日期 2017.01.19
申请号 US201514800346 申请日期 2015.07.15
申请人 Bell Helicopter Textron Inc. 发明人 Gillett, JR. Luke D.;Thomas Brandon J.;Schaeffer Joseph M.
分类号 G05D1/10;B64D31/06;B64C27/00 主分类号 G05D1/10
代理机构 代理人
主权项 1. A rotorcraft, comprising: a body; a power train coupled to the body and comprising one or more power sources and a drive shaft coupled to the one or more power sources; a rotor system coupled to the power train and comprising a plurality of rotor blades; a flight control system operable to change at least one operating condition of the rotor system; a pilot control device in communication with the flight control system and operable to receive a command from a pilot; a trim assembly in mechanical communication with the pilot control device and operable to apply a force against the pilot control device in resistance of the command from the pilot; and a trim assembly control system in communication with the trim assembly and configured to: identify a first pilot control device position relative to a reference pilot control device position; andinstruct the trim assembly to apply a cueing force against the pilot control device if the pilot control device is positioned proximate to the first pilot control device position.
地址 Fort Worth TX US