NDLI: Cooperative control with adaptive graph Laplacians for spacecraft formation flying

Content Provider	IEEE Xplore Digital Library
Author	Insu Chang Soon-Jo Chung Blackmore, L.
Copyright Year	2010
Description	Author affiliation: Department of Aerospace Engineering, University of Illinois at Urbana-Champaign, 61801, USA (Insu Chang; Soon-Jo Chung) \|\| Jet Propulsion Laboratory, California Institute of Technology, Pasadena, 91109, USA (Blackmore, L.)
Abstract	This paper investigates exact nonlinear dynamics and cooperative control for spacecraft formation flying with Earth oblateness (J2 perturbation) and atmospheric drag effects. The nonlinear dynamics for chief and deputy motions are derived by using Gauss' variational equation and the Euler-Lagrangian formulation, respectively. The proposed cooperative control employs adaptive time-varying Laplacian gains. The tracking and diffusive coupling gains are adapted by the synchronization/tracking errors and distance-based connectivity, thereby defining a time-varying network topology. Moreover, the proposed method relaxes the network structure requirement and permits an unbalanced graph. Nonlinear stability is proven by contraction analysis and incremental input-to-state stability. Numerical examples show the effectiveness of the proposed method.
Starting Page	4926
Ending Page	4933
File Size	763260
Page Count	8
File Format	PDF
ISBN	9781424477456
ISSN	07431546
e-ISBN	9781424477463
DOI	10.1109/CDC.2010.5717516
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2010-12-15
Publisher Place	USA
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Space vehicles Mathematical model Synchronization Equations Atmospheric modeling Couplings Aerodynamics
Content Type	Text
Resource Type	Article
Subject	Control and Optimization Control and Systems Engineering Modeling and Simulation

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