DocumentCode
3267071
Title
Coordinated orbit transfer for satellite clusters
Author
Zhang, Fhmin ; Krishnaprasad, P.S.
Author_Institution
Dept. of Electr. & Comput. Eng., Maryland Univ., College Park, MD, USA
Volume
4
fYear
2002
fDate
10-13 Dec. 2002
Firstpage
4095
Abstract
We propose a control law which allows a satellite formation to achieve orbit transfer. During the transfer, the formation can be either maintained or modified to a desired one. Based on the orbit transfer control law proposed by Chang, Chichka and Marsden (2002) for single satellite, we add coupling terms to the summation of Lyapunov functions for single satellites. These terms are functions of the difference between the mean anomalies (or perigee passing times) of formation members. The asymptotic stability of the desired formation in desired orbits is proved.
Keywords
Lyapunov methods; asymptotic stability; attitude control; space vehicles; Lyapunov functions; asymptotic stability; coordinated orbit transfer control; formation members; mean anomalies; perigee passing times; satellite clusters; satellite formation; Asymptotic stability; Control systems; Convergence; Earth; Educational institutions; Force control; Intelligent structures; Lyapunov method; Satellites; Space shuttles;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 2002, Proceedings of the 41st IEEE Conference on
ISSN
0191-2216
Print_ISBN
0-7803-7516-5
Type
conf
DOI
10.1109/CDC.2002.1185009
Filename
1185009
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