DocumentCode :
1641022
Title :
Generating optimised satellite payload operation schedules with Evolutionary Algorithms
Author :
Weber, Andreas ; Fasoulas, Stefanos ; Wolf, Klaus
Author_Institution :
Inst. of Aerosp. Eng., Tech. Univ. Dresden, Dresden
fYear :
2009
Firstpage :
2332
Lastpage :
2339
Abstract :
An optimised schedule is vital for the operation of an interplanetary space mission. The scheduling problem of a mission with the scientific objective of reaching global coverage with more than one instrument is complex and highly restricted. Evolutionary algorithms can be an efficient method in solving scheduling problems and generating pareto-optimal alternatives. The application of an algorithm combining evolutionary strategy, genetic algorithm and differential evolution is demonstrated for a reference scenario of a low-orbit Moon mapping mission. A reduced set of restrictions is taken into account for creating a master schedule for the operation of three different instruments for the whole mission time. An optimal set of short term operation time lines for one orbit is generated, which can be combined to a complete mission schedule. The results show that more than one year mission time can be saved with an optimised schedule.
Keywords :
artificial satellites; evolutionary computation; genetic algorithms; scheduling; differential evolution; evolutionary algorithms; genetic algorithm; interplanetary space mission; low-orbit Moon mapping mission; optimised satellite payload operation schedules; pareto-optimal alternatives; Aerospace engineering; Artificial satellites; Constraint optimization; Evolutionary computation; Instruments; Mars; Memory; Moon; Payloads; Satellite ground stations;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Evolutionary Computation, 2009. CEC '09. IEEE Congress on
Conference_Location :
Trondheim
Print_ISBN :
978-1-4244-2958-5
Electronic_ISBN :
978-1-4244-2959-2
Type :
conf
DOI :
10.1109/CEC.2009.4983231
Filename :
4983231
Link To Document :
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