发明名称 FLY BY WIRE SERVOS WITH INTERNAL LOOP CLOSURE
摘要 Embodiments are directed to obtaining a first analog signal corresponding to a position error between a commanded gang output of a plurality of electro-mechanical actuators configured to be run in parallel with one another and a measured gang output of the plurality of electro-mechanical actuators, obtaining a second analog signal corresponding to an output torque, and processing, by a circuit, the first analog signal and the second analog signal to generate and output a discrete that indicates a status of the torque in terms of direction and magnitude.
申请公布号 US2015360771(A1) 申请公布日期 2015.12.17
申请号 US201514835950 申请日期 2015.08.26
申请人 Sikorsky Aircraft Corporation 发明人 Cotton Bryan S.;Harrigan Matthew;Winslow Christopher L.
分类号 B64C13/50 主分类号 B64C13/50
代理机构 代理人
主权项 1. A servo assembly comprising: a hydraulic primary servo; and a plurality of electro-mechanical actuators coupled to the primary servo and configured to drive the primary servo; wherein the electro-mechanical actuators are configured to perform loop closure.
地址 Stratford CT US
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