发明名称 AIRCRAFT DYNAMIC PRESSURE ESTIMATION SYSTEM AND METHOD
摘要 Methods and apparatus are provided for estimating aircraft dynamic pressure. The load on the flight control surface actuator that is coupled to a flight control surface is measured. An estimate of the aircraft dynamic pressure is calculated from the measured load.
申请公布号 US2011202291(A1) 申请公布日期 2011.08.18
申请号 US20100705007 申请日期 2010.02.12
申请人 HONEYWELL INTERNATIONAL INC. 发明人 HICKMAN ALAN BRUCE
分类号 G01L7/00;G06F19/00 主分类号 G01L7/00
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