Spacecraft design using a genetic algorithm optimization approach

被引:0
|
作者
Mosher, T [1 ]
机构
[1] Univ Colorado, Redondo Beach, CA 90278 USA
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D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Spacecraft design is a highly coupled problem. The design of the spacecraft must balance payload objectives and orbital design against cost and schedule guidelines. Currently spacecraft are 'optimized' manually through a tool-assisted evaluation of a limited set of design alternatives. With this approach there is no guarantee that a system-level focus will be taken and 'feasibility' rather than 'optimality' is commonly all that is achieved.
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页码:123 / 134
页数:12
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