DocumentCode :
2183996
Title :
Formation and maneuver control of multiple spacecraft
Author :
Lee, Dongjun ; Li, Perry Y.
Author_Institution :
Dept. of Mech. Eng., Minnesota Univ., Minneapolis, MN, USA
Volume :
1
fYear :
2003
fDate :
4-6 June 2003
Firstpage :
278
Abstract :
In this paper, we propose a novel control scheme that enables a group of multiple spacecraft to maneuver according to a desired trajectory while the internal shape of the group is ensured to converge to a prescribed formation structure. The main innovation of this paper lies in the design of a special decomposition that decomposes the dynamics of the group into two parts: dynamics of the overall group motion (average system), and the dynamics of the group internal formation (shape system). In addition, the decomposition has the property that the energies of the average and shape systems preserve that of the original system. Thus, the maneuver of the group can be achieved by controlling the average system, while the formation control can be achieved by controlling the shape system. The proposed control scheme can also be extended hierarchically for multiple groups. Simulation is performed to show the efficacy of the proposed control.
Keywords :
aerospace control; control system synthesis; matrix decomposition; position control; space vehicles; average energy; average system control; desired trajectory; dynamic decomposition; formation control; formation structure; group internal formation; maneuver control; multiple spacecraft; overall group motion; shape system control; special decomposition design; Control systems; Feedback; Interferometry; Mechanical engineering; Physics; Robustness; Shape control; Space vehicles; Surveillance; Technological innovation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2003. Proceedings of the 2003
ISSN :
0743-1619
Print_ISBN :
0-7803-7896-2
Type :
conf
DOI :
10.1109/ACC.2003.1238951
Filename :
1238951
Link To Document :
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