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 |
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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 |