Satellite Payload Reconfiguration Optimisation: An ILP Model

  • Apostolos Stathakis
  • Grégoire Danoy
  • Pascal Bouvry
  • Gianluigi Morelli
Part of the Lecture Notes in Computer Science book series (LNCS, volume 7197)

Abstract

The increasing size and complexity of communication satellites has made the manual management of their payloads by engineers through computerised schematics difficult and error prone. This article proposes to optimise payload reconfigurations for current and next generation satellites using a novel Integer Linear Programming model (ILP), which is a variant of network flow models. Experimental results using CPLEX demonstrate the efficiency and scalability of the approach up to realistic satellite payloads sizes and configurations.

Keywords

Integer-Linear programming network optimisation satellite payload 

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Copyright information

© Springer-Verlag Berlin Heidelberg 2012

Authors and Affiliations

  • Apostolos Stathakis
    • 1
  • Grégoire Danoy
    • 2
  • Pascal Bouvry
    • 2
  • Gianluigi Morelli
    • 3
  1. 1.Interdisciplinary Centre for Security, Reliability, and TrustUniversity of LuxembourgLuxembourg
  2. 2.CSC Research UnitUniversity of LuxembourgLuxembourg
  3. 3.SES EngineeringBetzdorfLuxembourg

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