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.
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 代理人
主权项
地址