EFFECT OF TETHER FLEXIBILITY ON THE TETHERED SHUTTLE SUBSATELLITE STABILITY AND CONTROL

被引：18
作者：
LIU, LD
BAINUM, PM
机构：
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1989年 / 12卷 / 06期
关键词：
D O I：
10.2514/3.20493
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：866 / 873
页数：8
相关论文
共 13 条
[1]  
Armstrong E. S., 1980, ORACLS DESIGN SYSTEM
[2]   SHUTTLE-TETHERED SUBSATELLITE SYSTEM STABILITY WITH A FLEXIBLE MASSIVE TETHER [J].
BAINUM, PM ;
DIARRA, CM ;
KUMAR, VK .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1985, 8 (02) :230-234
[3]   OPTIMAL-CONTROL OF THE SHUTTLE-TETHERED-SUBSATELLITE SYSTEM [J].
BAINUM, PM ;
KUMAR, VK .
ACTA ASTRONAUTICA, 1980, 7 (12) :1333-1348
[4]  
BAINUM PM, 1978, NASA CR156976
[5]  
BAKER WP, 1976, NASA TMX73314
[6]  
BANERJEE AK, 1982, J ASTRONAUT SCI, V30, P347
[7]  
MISRA AK, 1980, ASTRODYNAMICS 1979 2, V40, P537
[8]  
MISRA AK, 1987, TETHERS SPACE ADV AS, V62, P667
[9]  
MISRA AK, 1986, AIAA862274 PAP
[10]   ON THE CONTROL OF THE SPACE-SHUTTLE BASED TETHERED SYSTEMS [J].
MODI, VJ ;
GENG, CF ;
MISRA, AK ;
DA, MX .
ACTA ASTRONAUTICA, 1982, 9 (6-7) :437-443
12