DocumentCode
630893
Title
Decentralized mean orbit element formation stability for uncoordinated maneuvers
Author
Holzinger, Marcus J. ; McMahon, Jay W.
Author_Institution
Sch. of Aerosp. Eng., Georgia Inst. of Technol., Atlanta, GA, USA
fYear
2013
fDate
17-19 June 2013
Firstpage
4814
Lastpage
4819
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.
Keywords
Lyapunov methods; aerospace control; decentralised control; motion control; position control; space vehicles; stability; Lyapunov stability formalisms; decentralized mean orbit element formation stability; distributed mean orbit element spacecraft formations; simultaneous uncoordinated impulsive maneuvers; sufficient stability conditions; uncoordinated maneuvers; Educational institutions; Equations; Kalman filters; Lyapunov methods; Orbits; Space vehicles; Stability analysis;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference (ACC), 2013
Conference_Location
Washington, DC
ISSN
0743-1619
Print_ISBN
978-1-4799-0177-7
Type
conf
DOI
10.1109/ACC.2013.6580583
Filename
6580583
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