DocumentCode :
2848383
Title :
An observer based distributed controller for formation flying of satellites
Author :
Menon, P.P. ; Edwards, C.
Author_Institution :
Math. Res. Inst., Univ. of Exeter, Exeter, UK
fYear :
2011
fDate :
June 29 2011-July 1 2011
Firstpage :
196
Lastpage :
201
Abstract :
In this paper, a novel nonlinear observer and controller framework is suggested for achieving formation control of a cluster of satellites. Exploiting the skew symmetry in the satellite dynamics, a novel nonlinear observer which has roots in the super-twist sliding mode observer is proposed. Estimation of the entire states and unknown bounded disturbances (and also faulty, corrupted leader control signals) in finite time is demonstrated using an elegant Lyapunov analysis. The proposed distributed controller is based on the state estimates and the relative position output information which depends on the underlying communication topology. The novelty in the synthesis of the controller is mainly in the treatment of the underlying graph topology, the interaction amongst the satellites in terms of relative sensing, and the synthesis of the controller gains using a simple polytopic representation that depends on the graph Laplacian eigenvalues. A simulation example is provided to demonstrate the efficacy of the proposed approach.
Keywords :
Lyapunov methods; artificial satellites; distributed control; graph theory; nonlinear control systems; observers; Lyapunov analysis; bounded disturbances; controller synthesis; graph Laplacian eigenvalues; graph topology; nonlinear observer; observer based distributed controller; polytopic representation; satellite dynamics; satellites formation flying; Equations; Mathematical model; Observers; Orbits; Position measurement; Satellite broadcasting; Satellites;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference (ACC), 2011
Conference_Location :
San Francisco, CA
ISSN :
0743-1619
Print_ISBN :
978-1-4577-0080-4
Type :
conf
DOI :
10.1109/ACC.2011.5990884
Filename :
5990884
Link To Document :
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