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导弹总体多学科设计优化耦合关系处理方法 被引量:6

Processing Methods of Coupled Relationship of Multidisciplinary Design Optimization for Missile
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摘要 导弹总体设计是一个复杂过程,涉及多个学科专业,这些学科之间又是相互联系、相互耦合和相互矛盾的,这就为优化每次迭代需要进行的系统分析带来了困难。针对导弹总体多学科设计优化中学科间耦合关系带来的系统分析困难,结合导弹总体设计提出了4种处理耦合关系的方法,并分析了这4种方法的特点。 Missile collectivity system design coupled and contradicted with each other. This may is a complex procedure, involving lots of subjects. These subjects are related, bring more difficulties on system analysis of multidisciplinary design optimization in every iteration. In order to tackle the difficulties of system analyzing which brought by coupled subjects, 4 methods for handling coupled system associating missile general design are given, and the characters of these method are analyzed.
出处 《导弹与航天运载技术》 北大核心 2009年第6期5-7,共3页 Missiles and Space Vehicles
关键词 耦合关系 多学科设计优化 系统分析 代理模型 导弹总体设计 Coupled relation Multidisciplinary design optimization System analysis Surrogate model Missile general design
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参考文献2

  • 1Sobieszczanski-Sobieski. A linear decomposition method for optimization problems-blueprint for development[R]. NASA 83248, 1982.
  • 2Braun R D. Development and application of the collaborative optimization architecture in a multidisciplinary design environment[R]. SLAM, 1996.

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