发明名称 |
Model-following control system using acceleration feedback |
摘要 |
A feedback system for reducing the effects of destabilizing forces in a vehicle (e.g. helicopter) by utilizing acceleration feedback data sensed by an acceleration sensor located in the vehicle. This sensed acceleration signal is passed through a low-pass filter and combined with a command signal to produce an error signal. The error signal is multiplied by a predetermined gain to produce a corrective signal that is utilized by actuators to adjust an adjustable surface, such as a swashplate, on the vehicle.
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申请公布号 |
US6189836(B1) |
申请公布日期 |
2001.02.20 |
申请号 |
US19980160598 |
申请日期 |
1998.09.25 |
申请人 |
SIKORSKY AIRCRAFT CORPORATION |
发明人 |
GOLD PHILLIP JEREMY;MAYO JOHN RANDALL |
分类号 |
G05D1/08;(IPC1-7):G05D1/00 |
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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