LARGE SPACE TELESCOPE OSCILLATIONS INDUCED BY CMG FRICTION

被引:7
作者
SELTZER, SM [1 ]
机构
[1] NASA,SYST DYNAM LAB,POINTING CONTROL SYST BRANCH,MARSHALL SP FLIGHT CTR,HUNTSVILLE,AL 35812
关键词
D O I
10.2514/3.27815
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:96 / 105
页数:10
相关论文
共 16 条
[1]  
ANDRONOW A, 1949, THEORY OSCILLATIONS, P203
[2]   METHOD OF EARTH-POINTING ATTITUDE-CONTROL FOR ELLIPTIC ORBITS [J].
CONNELL, GM .
AIAA JOURNAL, 1972, 10 (03) :258-&
[3]  
DAHL PR, 1968, TOR158310718 AER COR
[4]  
FRIEDER M, 1972, MT15 BEND CORP ENG F
[5]  
Gelb A., 1968, MULTIPLE INPUT DESCR
[6]  
KUO BC, TO BE PUBLISHED
[7]  
KUO BC, 1974, AIAA74874 PAP
[8]   PRECISION CMG CONTROL FOR HIGH-ACCURACY POINTING [J].
LIDEN, SP .
JOURNAL OF SPACECRAFT AND ROCKETS, 1974, 11 (04) :236-240
[9]  
OGATA K, 1970, MODERN CONTROL ENGIN, P585
[10]  
RYBAK SC, 1971, RAMBGNC407 BEND CORP