发明名称 Flight control system installed in aircraft cockpit continuously monitors flight parameters with evaluation via fuzzy logic for controlling pilot information display
摘要 The flight control system (1) automatically detects safety critical flight parameters and provides the aircraft pilot with the necessary information for correcting the flight parameters via a cockpit display. A computer operates in parallel with the flight regulation and uses a fuzzy logic (2) for safety risk evaluation of the monitored flight data parameters.
申请公布号 DE10046007(C1) 申请公布日期 2001.10.31
申请号 DE20001046007 申请日期 2000.09.18
申请人 EADS DEUTSCHLAND GMBH 发明人 WESTPHAL, PETER
分类号 B64D43/00;G05D1/00;(IPC1-7):B64D43/02 主分类号 B64D43/00
代理机构 代理人
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