Abstract:
This paper presents a discrete time sliding mode control system based upon a discrete reaching rate law and applied to an autonomous 6DoF satellite cluster located at the...Show MoreMetadata
Abstract:
This paper presents a discrete time sliding mode control system based upon a discrete reaching rate law and applied to an autonomous 6DoF satellite cluster located at the interior Sun-Earth Lagrange point. Centralized decision processes with distributed action are used to enable cluster dispersal from a central spacecraft and reconfiguration to optimally form an interferometer array dependant upon the number of cluster members, whilst considering collision avoidance.
Published in: 2009 European Control Conference (ECC)
Date of Conference: 23-26 August 2009
Date Added to IEEE Xplore: 02 April 2015
Print ISBN:978-3-9524173-9-3