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