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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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