On the capture of tumbling satellite by a space robot

被引:70
作者
Yoshida, Kazuya [1 ]
Dimitrov, Dimitar [1 ]
Nakanishi, Hiroki [1 ]
机构
[1] Tohoku Univ, Dept Aerosp Engn, Sendai, Miyagi 980, Japan
来源
2006 IEEE/RSJ INTERNATIONAL CONFERENCE ON INTELLIGENT ROBOTS AND SYSTEMS, VOLS 1-12 | 2006年
关键词
D O I
10.1109/IROS.2006.281900
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper deals with problems related to the capture of a tumbling satellite by a space robot. The minimization of the base attitude deviation before and after the contact with the target is discussed from the viewpoint of angular momentum distribution. By using the bias momentum approach during the approaching phase, impedance control during the impact, and distributed momentum control during the post-impact phase, we propose a possible control sequence for the successful completion of a capturing operation.
引用
收藏
页码:4127 / +
页数:2
相关论文
共 34 条
[1]   A new laboratory simulator for study of motion of free-floating robots relative to space targets [J].
Agrawal, SK ;
Hirzinger, G ;
Landzettel, K ;
Schwertassek, R .
IEEE TRANSACTIONS ON ROBOTICS AND AUTOMATION, 1996, 12 (04) :627-633
[2]   Design and experiments on a free-floating planar robot for optimal chase and capture operations in space [J].
Annapragada, M ;
Agrawal, SK .
ROBOTICS AND AUTONOMOUS SYSTEMS, 1999, 26 (04) :281-297
[3]   DYNAMICAL MODELING AND CONTROL OF A SPACECRAFT-MOUNTED MANIPULATOR CAPTURING A SPINNING SATELLITE [J].
CYRIL, X ;
JAAR, GJ ;
MISRA, AK .
ACTA ASTRONAUTICA, 1995, 35 (2-3) :167-174
[4]  
CYRIL X, 1993, P IEEE RSJ INT C INT, P2070
[5]  
DICKSON C, 1995, P IEEE RSJ INT C INT, P51
[6]  
Dimitrov D., 2004, P IEEE RSJ INT C INT, P3345
[7]  
DIMITROV D, 2006, THESIS TOHOKU U
[8]  
Inaba N., 2000, P IEEE RSJ INT C INT, V2, P1169, DOI DOI 10.1109/ROBOT.2000.844757
[9]  
JAAR G, 1992, 43 C INT ASTR FED
[10]  
Jacobsen S., 2002, P ASME 27 ANN BIENN