AN ANALYTICAL AND EXPERIMENTAL-STUDY OF A CONTROL-SYSTEMS SENSITIVITY TO STRUCTURAL MODIFICATIONS

被引：9

作者：

HAFTKA, RT

MARTINOVIC, ZN

HALLAUER, WL

SCHAMEL, G

机构：

[1] Virginia Polytechnic Inst &, State Univ, Blacksburg, VA, USA, Virginia Polytechnic Inst & State Univ, Blacksburg, VA, USA

来源：

AIAA JOURNAL | 1987年 / 25卷 / 02期

基金：

美国国家航空航天局;

关键词：

CRUCIFORM BEAM MODEL - STRUCTURAL MODIFICATIONS;

D O I：

10.2514/3.9623

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：310 / 315

页数：6

共 17 条

[1]

AUBRUN JN, 1984, J GUID CONTROL DYNAM, V7, P535, DOI 10.2514/3.19892

[2]

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[3] ENHANCED VIBRATION CONTROLLABILITY BY MINOR STRUCTURAL MODIFICATIONS [J].

HAFTKA, RT ;

MARTINOVIC, ZN ;

HALLAUER, WL .

AIAA JOURNAL, 1985, 23 (08) :1260-1266

[4]

HAFTKA RT, 1984, AIAA841036 PAP

[5]

HAFTKA RT, 1985, ELEMENTS STRUCTURAL, P181

[6] OPTIMAL SIMULTANEOUS STRUCTURAL AND CONTROL DESIGN OF MANEUVERING FLEXIBLE SPACECRAFT [J].

HALE, AL ;

LISOWSKI, RJ ;

DAHL, WE .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1985, 8 (01) :86-93

[7]

HANKS BR, 1983, 24TH P AIAA STRUCT S

[8]

HORNER GC, 1983, 24H P AIAA ASME ASCE, P179

[9]

KAMMER DC, 1979, 2ND VPI SU AIAA S DY

[10]

KHOT NS, 1984, AIAA840997 PAP

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