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

页码：123 / 134

页数：12

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