DocumentCode
2113383
Title
Evolutionary computing for spacecraft power subsystem design search and optimization
Author
Kordon, Mark ; Klimeck, Gerhard ; Hanks, David ; Hua, Hook
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume
6
fYear
2004
fDate
6-13 March 2004
Firstpage
4004
Abstract
Evolutionary computing has proven to be a straightforward and robust approach for optimizing a wide range of difficult analysis and design problems. This paper discusses the application of these techniques to an existing space vehicle power subsystem resource and performance simulation in a parallel processing environment. Using this method, engineers can trade off subsystem goals of mass, cost and performance then automatically size power elements based on their anticipated performance. Our results show that this approach has the potential to improve the space system trade study process.
Keywords
aerospace instrumentation; aerospace simulation; evolutionary computation; parallel processing; power system CAD; search problems; space vehicle power plants; evolutionary computation; optimization; parallel processing environment; performance simulation; power subsystem resource; search problems; space system trade study process; spacecraft power subsystem design; Computational modeling; Costs; Design optimization; Laboratories; Payloads; Power engineering computing; Project management; Propulsion; Space technology; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2004. Proceedings. 2004 IEEE
ISSN
1095-323X
Print_ISBN
0-7803-8155-6
Type
conf
DOI
10.1109/AERO.2004.1368219
Filename
1368219
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