MAXIMUM-LIKELIHOOD FAILURE-DETECTION OF AIRCRAFT FLIGHT CONTROL SENSORS

被引：7

作者：

FRIEDLAND, B

机构：

来源：

关键词：

D O I：

10.2514/3.19782

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：498 / 503

页数：6

共 11 条

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[2]

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[3]

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[4]

CHIEN TT, 1976, IEEE T AUTOMAT CONTR, V21, P750, DOI 10.1109/TAC.1976.1101363

[5] F-8 DFBW SENSOR FAILURE IDENTIFICATION USING ANALYTIC REDUNDANCY [J].

DECKERT, JC ;

DESAI, MN ;

DEYST, JJ ;

WILLSKY, AS .

FRIEDLAND, B .

[7] SEPARATE-BIAS ESTIMATION [J].

FRIEDLAND, B .

FRIEDLAND, B .

[9] ESTIMATING SUDDEN CHANGES OF BIASES IN LINEAR DYNAMIC-SYSTEMS [J].

FRIEDLAND, B ;

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[10]

Wald Abraham, 1947, SEQUENTIAL ANAL