COMPENSATING STRUCTURE AND PARAMETER OPTIMIZATION FOR ATTITUDE-CONTROL OF A FLEXIBLE SPACECRAFT

被引：2

|

作者：

CEBALLOS, DC

机构：

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1986年 / 9卷 / 02期

关键词：

D O I：

10.2514/3.20097

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

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页码：248 / 249

页数：2

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