MODIFIED INDEPENDENT MODAL SPACE CONTROL METHOD FOR ACTIVE CONTROL OF FLEXIBLE SYSTEMS

被引：11

作者：

BAZ, A ^{[1
]}

POH, S ^{[1
]}

STUDER, P ^{[1
]}

机构：

[1] NASA,GODDARD SPACE FLIGHT CTR,GREENBELT,MD 20771

来源：

关键词：

D O I：

10.1243/PIME_PROC_1989_203_093_02

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

引用

页码：103 / 112

页数：10

共 12 条

[1] FEEDBACK-CONTROL OF FLEXIBLE SYSTEMS [J].

BALAS, MJ .

[2]

CORADETTI T, 1979, AUG AIAA C GUID CONT

[3]

Meirovitch L., 1980, Journal of Guidance and Control, V3, P140, DOI 10.2514/3.55961

[4] CONTROL OF SPINNING FLEXIBLE SPACECRAFT BY MODAL SYNTHESIS [J].

MEIROVITCH, L ;

VANLANDINGHAM, HF ;

OZ, H .

[5] OPTIMAL-CONTROL OF DAMPED FLEXIBLE GYROSCOPIC SYSTEMS [J].

MEIROVITCH, L ;

BARUH, H .

JOURNAL OF GUIDANCE AND CONTROL, 1981, 4 (02) :157-163

[6]

MEIROVITCH L, 1979, DEC IEEE C DEC CONTR, P220

[7]

MEIROVITCH L, 1980, AUG AIAA C GUID CONT

[8]

Oz H., 1980, Journal of Guidance and Control, V3, P218, DOI 10.2514/3.55975

[9]

PORTER B, 1972, MODAL CONTROL THEORY

[10]

SESAK JR, 1979, 2ND P VPI SUAIAA S D