ATTITUDE DYNAMICS OF A SATELLITE DURING DEPLOYMENT OF LARGE PLATE-TYPE STRUCTURES

被引：17

作者：

IBRAHIM, AE

MISRA, AK

机构：

来源：

关键词：

D O I：

10.2514/3.56192

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：442 / 447

页数：6

共 14 条

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HUGHES PC, 1972, C A S I TRANS, V5, P11

[7]

IBRAHIM AE, 1981, THESIS MCGILL U MONT

[8]

LANG W, 1967, NASA TND4074

[9]

Leissa A, 1969, VIBRATION PLATES

LIPS, KW ;

MODI, VJ .

JOURNAL OF GUIDANCE AND CONTROL, 1981, 4 (06) :650-656