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Preliminary Design of a Manned Nuclear Electric Propulsion Vehicle Using Genetic Algorithms
Author(s) -
Ryan W. Irwin,
Michael Tinker
Publication year - 2005
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.177
H-Index - 75
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/1.1867223
Subject(s) - propulsion , conceptual design , genetic algorithm , computer science , computation , electrically powered spacecraft propulsion , selection (genetic algorithm) , mars exploration program , algorithm design , fitness function , algorithm , aerospace engineering , engineering , artificial intelligence , machine learning , astronomy , human–computer interaction , physics
Nuclear electric propulsion (NEP) vehicles will be needed for future manned missions to Mars and beyond. Candidate designs must be identified for further detailed design from a large array of possibilities. Genetic algorithms have proven their utility in conceptual design studies by effectively searching a large design space to pinpoint unique optimal designs. This research combined analysis codes for NEP subsystems with a genetic algorithm. The use of penalty functions with scaling ratios was investigated to increase computational efficiency. Also, the selection of design variables for optimization was considered to reduce computation time without losing beneficial design search space. Finally, trend analysis of a reference mission to the asteroids yielded a group of candidate designs for further analysis.

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