DocumentCode :
1871332
Title :
Application of an incremental evolution technique to spacecraft design optimization
Author :
Fukunaga, Alex S.
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear :
1997
fDate :
13-16 Apr 1997
Firstpage :
431
Lastpage :
435
Abstract :
Based on the intuition that it is often easier to learn to solve difficult problems after similar, simpler problems have been learned, incremental evolution is an extension to evolutionary algorithms in which the evaluation function against which a population is evolved is scaled over time. This paper presents an application of incremental evolution to the problem of physical design optimization of a Mars microprobe spacecraft. Experimental results that demonstrated the utility of the approach are presented, as well as some new insights into the behavior of incremental evolution which may explain its success
Keywords :
CAD; Mars; aerospace computing; genetic algorithms; space vehicles; Mars microprobe spacecraft; evaluation function; evolutionary algorithms; incremental evolution technique; population; problem solving; spacecraft design optimization; Design optimization; Evolution (biology); Evolutionary computation; Genetic algorithms; Mars; Optimization methods; Psychology; Scheduling; Space exploration; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Evolutionary Computation, 1997., IEEE International Conference on
Conference_Location :
Indianapolis, IN
Print_ISBN :
0-7803-3949-5
Type :
conf
DOI :
10.1109/ICEC.1997.592350
Filename :
592350
Link To Document :
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