Formation Flying Control of Multiple Spacecraft via Graphs, Matrix Inequalities, and Switching

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Abstract

Ideas from elementary graph theory and linear matrix inequalities are combined with logic-based switching to shed light on the various control strategies which are feasible in the leader-following framework for the formation flying of multiple spacecraft.

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Authors

Mehran Mesbahi

University of Washington

Fred Y. Hadaegh

California Institute of Technology

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Journal of Guidance Control and Dynamics

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University of Minnesota

California Institute of Technology

Jet Propulsion Laboratory

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Mesbahi et al. (Thu,) studied this question.

synapsesocial.com/papers/6a0eadab1c5e2d2319f9b5c8 — DOI: https://doi.org/10.2514/2.4721

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Also consider

Synapse has enriched 5 closely related papers on similar clinical questions. Consider them for comparative context:

Synchronized Formation Rotation and Attitude Control of Multiple Free-Flying Spacecraft· 1999 · 262 citations
The Journal of the Astronautical Sciences· 2013 · 2,786 citations
Society for Industrial and Applied Mathematics· 1973 · 902 citations
Linear Matrix Inequalities in System and Control Theory· 1994 · 21,490 citations
Interior-Point Polynomial Algorithms in Convex Programming· 1994 · 4,340 citations

Formation Flying Control of Multiple Spacecraft via Graphs, Matrix Inequalities, and Switching

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