DocumentCode
1232555
Title
SSME parameter model input selection using genetic algorithms
Author
Peck, Charles C. ; Dhawan, Atam P.
Author_Institution
TASC, Arlington, VA, USA
Volume
32
Issue
1
fYear
1996
Firstpage
199
Lastpage
212
Abstract
Genetic algorithms are used for the systematic selection of inputs for a parameter modeling system based on a neural network function approximator. Due to the nature of the underlying system, issues such as learning, generalization, exploitation, and robustness are also examined. In the application considered, modeling critical parameters of the Space Shuttle Main Engine (SSME), the functional relationships among measured parameters are unknown and complex. Furthermore, the number of possible input parameters is quite large. Many approaches have been proposed for input selection, but they are either not possible due to insufficient instrumentation, are subjective, or they do not consider the complex multivariate relationships between parameters. Due to the optimization and space searching capabilities of genetic algorithms, they were employed in this study to systematize the input selection process. The results suggest that the genetic algorithm can generate parameter lists of high quality without the explicit use of problem domain knowledge.
Keywords
aerospace propulsion; aerospace simulation; digital simulation; genetic algorithms; learning (artificial intelligence); neural nets; parameter estimation; rocket engines; space vehicles; SSME; Space Shuttle Main Engine; genetic algorithms; input selection process; learning; multivariate relationships; neural network function approximator; parameter lists; parameter model input selection; robustness; rocket engine condition monitoring; space searching capabilities; Engines; Equations; Genetic algorithms; Instruments; Neural networks; Real time systems; Robustness; Rockets; Space shuttles; Space technology;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/7.481262
Filename
481262
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