TY - GEN
T1 - Utilization of the bias momentum approach for capturing a tumbling satellite
AU - Dimitrov, Dimitar Nikolaev
AU - Yoshida, Kazuya
PY - 2004/12/1
Y1 - 2004/12/1
N2 - This paper deals with problems related to the capture of a tumbling satellite by a space robot. The minimization of the base attitude deviation after the contact with the target is discussed from the viewpoint of angular momentum distribution. A new capturing strategy utilizing bias momentum is introduced. By using the null space of the coupling inertia matrix we present a method for angular momentum redistribution while following a desired trajectory.
AB - This paper deals with problems related to the capture of a tumbling satellite by a space robot. The minimization of the base attitude deviation after the contact with the target is discussed from the viewpoint of angular momentum distribution. A new capturing strategy utilizing bias momentum is introduced. By using the null space of the coupling inertia matrix we present a method for angular momentum redistribution while following a desired trajectory.
UR - http://www.scopus.com/inward/record.url?scp=14044252313&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=14044252313&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:14044252313
SN - 0780384636
T3 - 2004 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS)
SP - 3333
EP - 3338
BT - 2004 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS)
T2 - 2004 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS)
Y2 - 28 September 2004 through 2 October 2004
ER -