Constraint-Based Random Search for Solving Spacecraft Downlink Scheduling Problems. In Selected papers from the 1st Multidisciplinary International Conference on Scheduling: Theory and Applications (MISTA), pages 133-160, Springer, 2005.
Selected
This paper introduces a combinatorial optimisation problem called the Mars Express Memory Dumping Problem (Mex-Mdp), which arises in the European Space Agency programme Mars Express. The domain is characterized by complex constraints concerning bounded on-board memory capacities, limited communication windows over the downlink channels, deadlines and ready times imposed by the scientists using the spacecraft instruments. This paper lays out the problem and analyses its computational complexity showing that Mex-Mdp is NP-hard. Then the problem is modelled as a Constraint Satisfaction Problem and two different heuristic strategies for its solution are presented: a core greedy constraint-based procedure and an iterative sampling strategy based on random search. The algorithms are evaluated both against a benchmark set created on the basis of ESA documentation and a lower bound of the minimised objective function. Experimental results show the overall effectiveness of the approach.
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@INBOOK{2005-133-160-SI, chapter = {Selected papers from the 1st Multidisciplinary International Conference on Scheduling: Theory and Applications (MISTA)},
pages = {133--160},
title = {Constraint-Based Random Search for Solving Spacecraft Downlink Scheduling Problems},
publisher = {Springer},
year = {2005},
editor = {G. Kendall and E. Burke and S. Petrovic and M. Gendreau},
author = {A. Oddi and N. Policella and A. Cesta and G. Cortellessa},
note = {Selected},
abstract = {This paper introduces a combinatorial optimisation problem called the Mars Express Memory Dumping Problem (Mex-Mdp), which arises in the European Space Agency programme Mars Express. The domain is characterized by complex constraints concerning bounded on-board memory capacities, limited communication windows over the downlink channels, deadlines and ready times imposed by the scientists using the spacecraft instruments. This paper lays out the problem and analyses its computational complexity showing that Mex-Mdp is NP-hard. Then the problem is modelled as a Constraint Satisfaction Problem and two different heuristic strategies for its solution are presented: a core greedy constraint-based procedure and an iterative sampling strategy based on random search. The algorithms are evaluated both against a benchmark set created on the basis of ESA documentation and a lower bound of the minimised objective function. Experimental results show the overall effectiveness of the approach.},
doi = {10.1007/0-387-27744-7_7},
owner = {gxk},
timestamp = {2012.05.29} }