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
来源：
1998 IEEE AEROSPACE CONFERENCE PROCEEDINGS, VOL. 3 | 1998年
关键词：
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.
引用
收藏
页码：123 / 134
页数：12
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