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.
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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 |
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代理人 |
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主权项 |
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地址 |
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