Decentralized Mean Orbit-Element Formation Stability for Uncoordinated Maneuvers
Author(s)
Holzinger, Marcus J.
McMahon, Jay W.
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Abstract
Sufficient stability conditions are derived for simultaneous
uncoordinated impulsive maneuvers in distributed
mean orbit element spacecraft formations. Lyapunov stability
formalisms are used in conjunction with distributed mean orbit
element spacecraft formation definitions. Special cases of the
sufficient stability conditions are examined. Simulated results
demonstrate the efficacy of the approach, and conclusions and
future work are discussed.
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Date
2013-06
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Text
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Paper
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