BANG-BANG CONTROL OF FLEXIBLE SPACECRAFT SLEWING MANEUVERS - GUARANTEED TERMINAL POINTING ACCURACY

被引：22

作者：

SINGH, G ^{[1
]}

KABAMBA, PT ^{[1
]}

MCCLAMROCH, NH ^{[1
]}

机构：

[1] UNIV MICHIGAN,DEPT AEROSP ENGN,ANN ARBOR,MI 48109

来源：

关键词：

D O I：

10.2514/3.56512

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

[No abstract available]

引用

页码：376 / 379

页数：4

共 9 条

[1]

[Anonymous], 1981, PATHWAYS SOLUTIONS F

[2]

BARBIERI E, 1988, IN PRESS 27TH C DEC

[3]

BENASHER J, 1987, 26TH P C DEC CONTR L

HUGHES, PC .

JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1980, 47 (01) :177-184

SINGH, G ;

KABAMBA, PT ;

MCCLAMROCH, NH .

[6]

SINGH G, 1988, THESIS U MICHIGAN AN

[7] ON-OFF ATTITUDE-CONTROL OF FLEXIBLE SATELLITES [J].

SKAAR, SB ;

TANG, L ;

YALDAMOOSHABAD, I .

[8]

THOMPSON RC, 1987, AIAA870958CP PAP

[9]

VANDERVELDE W, 1983, J GUIDANCE CONTROL D, V6, P759