RESULTS OF NUMERICAL DETERMINATION OF POLES AND ZEROS OF A TRANSFER-FUNCTION FOR FLEXIBLE SPACECRAFT ATTITUDE-CONTROL

被引：0

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作者：

OHKAMI, Y

LIKINS, PW

机构：

[1] NATL AEROSP LAB,TOKYO,JAPAN

[2] COLUMBIA UNIV,NEW YORK,NY 10027

来源：

JOURNAL OF THE ASTRONAUTICAL SCIENCES | 1976年 / 24卷 / 04期

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D O I：

暂无

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：311 / 328

页数：18

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[1] DETERMINATION OF POLES AND ZEROS OF TRANSFER-FUNCTIONS FOR FLEXIBLE SPACECRAFT ATTITUDE-CONTROL
OHKAMI, Y
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[8] PROBLEMATIC OF THE DETERMINATION OF ZEROS AND POLES OF A TRANSFER-FUNCTION, WHICH IS DESCRIBED THROUGH A POLAR CURVE
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[J]. NTZ ARCHIV, 1983, 5 (06): : 179 - 184
[9] MULTIAXIS TRACKING AND ATTITUDE-CONTROL OF FLEXIBLE SPACECRAFT WITH REACTION JETS
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[J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1994, 17 (04) : 831 - 839
[10] ROBUST BEAM-POINTING AND ATTITUDE-CONTROL OF A FLEXIBLE SPACECRAFT
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[J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1986, 9 (02) : 228 - 234