Impulsive formation control using orbital energy and angular momentum vector

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This paper presents a multi-impulsive formation control strategy using orbit energy-matching and relative angular momentum vector between leader and follower satellites. These conservative parameters (energy and angular momentum) provide analytical and global solutions for orbital maneuver design without relying on Gauss variational equations. The relationship with orbit element differences is discussed in the simplifying assumptions. The proposed approach is free from small variation assumptions, so that it is suitable for handling even the case of large error corrections. General limitations of impulse control and associated compensation maneuvers are also addressed. (C) 2010 Elsevier Ltd. All rights reserved.
Publisher
PERGAMON-ELSEVIER SCIENCE LTD
Issue Date
2010-09
Language
English
Article Type
Article
Keywords

RELATIVE MOTION; SPACECRAFT FORMATIONS; ELLIPTIC ORBITS; ELEMENTS; DESIGN

Citation

ACTA ASTRONAUTICA, v.67, no.5-6, pp.613 - 622

ISSN
0094-5765
DOI
10.1016/j.actaastro.2010.04.008
URI
http://hdl.handle.net/10203/95542
Appears in Collection
AE-Journal Papers(저널논문)
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