CONTROL OF SPINNING FLEXIBLE SPACECRAFT BY MODAL SYNTHESIS

被引：17

作者：

MEIROVITCH, L ^{[1
]}

VANLANDINGHAM, HF ^{[1
]}

OZ, H ^{[1
]}

机构：

[1] VIRGINIA POLYTECH INST & STATE UNIV,DEPT ELECT ENGN,BLACKSBURG,VA 24061

来源：

关键词：

D O I：

10.1016/0094-5765(77)90002-9

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：985 / 1010

页数：26

共 7 条

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[2]

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[3] INTRODUCTION TO OBSERVERS [J].

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[5] MODAL ANALYSIS FOR RESPONSE OF LINEAR GYROSCOPIC SYSTEMS [J].

MEIROVITCH, L .

JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1975, 42 (02) :446-450

[6]

POELAERT D, 1975, ESA SCI TECHNOL REV, V1, P203

[7] ATTITUDE-CONTROL OF FLEXIBLE SPACE-VEHICLES [J].

PORCELLI, G .