REDUCED-ORDER OPTIMAL FEEDBACK-CONTROL LAW SYNTHESIS FOR FLUTTER SUPPRESSION

被引：30

作者：

MUKHOPADHYAY, V

NEWSOM, JR

ABEL, I

机构：

来源：

关键词：

D O I：

10.2514/3.56187

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：389 / 395

页数：7

共 13 条

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[2] ABEL I, 1979, AIAA791633 PAP
[3] Armstrong E. S., 1980, ORACLS DESIGN SYSTEM
[4] ROBUSTNESS WITH OBSERVERS
DOYLE, JC
STEIN, G
[J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1979, 24 (04) : 607 - 611
[5] GANGSAAS D, 1979, AIAA791746 PAP
[6] KWAKERNAAK K, 1972, LINEAR OPTIMAL CONTR, P427
[7] OPTIMAL LIMITED STATE VARIABLE FEEDBACK CONTROLLERS FOR LINEAR SYSTEMS
LEVINE, WS
JOHNSON, TL
ATHANS, M
[J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1971, AC16 (06) : 785 - &
[8] MAHESH JK, 1979, NASA CR159160, V1
[9] MARTIN GD, 1978, AIAA781281 PAP
[10] MUKHOPADHYAY V, 1981, NASA TP1876