MAGNETIC ATTITUDE CONTROL SYSTEM FOR AN AXISYMMETRIC SPINNING SPACECRAFT

被引:16
作者
SORENSEN, JA
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10.2514/3.59677
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V [航空、航天];
学科分类号
08 ; 0825 ;
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页码:441 / &
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共 11 条
[1]  
Bryson A, 1969, APPL OPTIMAL CONTROL, P148
[2]  
FISCHELL RE, 1966, PEACEFUL USES AUTOMA, P211
[3]  
HECHT E, 1964, TORQUES ATTITUDE SEN, P127
[4]  
LANGE BO, 1967, J SPACECRAFT ROCKETS, V4, P142
[5]  
MOORE JB, 1967, TREE6708 U NEWC DEP
[6]  
SONNABEND D, 1967, TR015833070116 REPT, P121
[7]  
SORENSEN JA, 1969, SUDAAR380
[8]  
VRABLIK EA, 1965, TN196548 MASS I TECH
[9]   SPINNING SPACECRAFT ATTITUDE CONTROL VIA ENVIRONMENTAL MAGNETIC FIELD [J].
WHEELER, PC .
JOURNAL OF SPACECRAFT AND ROCKETS, 1967, 4 (12) :1631-&
[10]   SPIN DECAY, SPIN-PRECESSION DAMPING, AND SPIN-AXIS DRIFT OF TELSTAR SATELLITE [J].
YU, EY .
BELL SYSTEM TECHNICAL JOURNAL, 1963, 42 (05) :2169-+