发明名称 Combined series and parallel servo control for aircraft
摘要 A flight control system increases the automatic control authority over, preferably, a helicopter yaw axis. A limited authority series servo is complemented with a full authority parallel servo. The parallel servo is driven by a combination of a trim command signal and a signal representing the excess of the yaw command signal over the amplitude limited drive signal to the series servo.
申请公布号 US4492907(A) 申请公布日期 1985.01.08
申请号 US19820393166 申请日期 1982.06.28
申请人 ROCKWELL INTERNATIONAL CORPORATION 发明人 FABIAN, GORDON R.;MCELREATH, KENNETH W.
分类号 G05D1/08;(IPC1-7):G05D1/08 主分类号 G05D1/08
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