Dynamics and control of a tethered space robot with tension

被引:0
作者
Hokamoto, S [1 ]
Imamura, N [1 ]
Modi, VJ [1 ]
机构
[1] Kyushu Univ, Dept Aeronaut & Astronaut, Higashi Ku, Fukuoka 8128581, Japan
来源
ASTRODYNAMICS 2001, PTS I-III | 2001年 / 109卷
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Whereas most of the previous studies treat free-floating space robots, this investigation deals with a space robot subjected to a tether tension force. The system is composed of a main satellite in orbit, a tether, and a space robot with a manipulator consisting of two connected links. This study explores coupled motions of the space robot, tether, and main satellite in a gravity-gradient field. Typical dynamics and control results obtained numerically are compared with those for a free-floating space robot.
引用
收藏
页码:1587 / 1595
页数:9
相关论文
共 5 条
[1]  
BANERJEE AK, 1982, J ASTRONAUT SCI, V30, P347
[2]  
FERNANDES C, 1993, OPTIMAL NONHOLONOMIC, P379
[3]   NONHOLONOMIC PATH PLANNING OF SPACE ROBOTS VIA A BIDIRECTIONAL APPROACH [J].
NAKAMURA, Y ;
MUKHERJEE, R .
IEEE TRANSACTIONS ON ROBOTICS AND AUTOMATION, 1991, 7 (04) :500-514
[4]  
SHABANA AA, 1990, THEORY VIBRATION, V2, pCH4
[5]  
VAFA Z, 1990, J ASTRONAUT SCI, V38, P441