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An Evolutionary Optimization System for Spacecraft Design

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dc.contributor.author Fukunaga, A. en_US
dc.contributor.author Stechert, A. en_US
dc.date.accessioned 2004-09-25T23:57:02Z
dc.date.available 2004-09-25T23:57:02Z
dc.date.issued 1997-06-10 en_US
dc.identifier.citation Atlanta, Georgia, USA en_US
dc.identifier.clearanceno 97-0237 en_US
dc.identifier.uri http://hdl.handle.net/2014/21833
dc.description.abstract Spacecraft design optimization is a domian that can benefit from the application of optimization algorithms such as genetic algorithms. In this paper, we describe DEVO, an evolutionary optimization system that addresses these issues and provides a tool that can be applied to a number of real-world spacecraft design applications. We describe two current applications of DEVO: physical design if a Mars Microprobe Soil Penetrator, and system configuration optimization for a Neptune Orbiter. en_US
dc.format.extent 622895 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other spacecraft design optimization DEVO Mars Microprobe Soil Penetrator Neptune Orbiter optimization algorithms en_US
dc.title An Evolutionary Optimization System for Spacecraft Design en_US


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