RECONFIGURABLE FLIGHT CONTROL VIA MULTIPLE MODEL ADAPTIVE-CONTROL METHODS

被引：135

作者：

MAYBECK, PS ^{[1
]}

STEVENS, RD ^{[1
]}

机构：

[1] USAF,WRIGHT RES & DEV CTR,AVION LAB,WRIGHT PATTERSON AFB,OH 45433

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 1991年 / 27卷 / 03期

关键词：

D O I：

10.1109/7.81428

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A multiple model adaptive controller (MMAC) is shown to provide effective reconfigurability when subjected to single and double failures of sensors and/or actuators. Its performance is enhanced by an alternate computation of the MMAC hypothesis probabilities, use of maximum a posteriori probability (MAP) versus Bayesian form of the MMAC (or a modified combination of both), and reduction of identification ambiguities through scalar residual monitoring for the case of sensor failures.

引用

页码：470 / 480

页数：11

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