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基于近似模型管理的微小卫星结构多目标优化设计

郑侃 廖文和 张翔

中国机械工程2012,Vol.23Issue(6):655-659,5.
中国机械工程2012,Vol.23Issue(6):655-659,5.

基于近似模型管理的微小卫星结构多目标优化设计

Multi--objective Optimization Design for Microsatellite Structure Based on Approximation Model Management

郑侃 1廖文和 1张翔1

作者信息

  • 1. 南京航空航天大学,南京210016
  • 折叠

摘要

Abstract

Aecording to the characteristics of multi--objective optimization for microsatellite structure, a new method for approximation model management was presented based on the trust region. Orthogonal and Kriging approximate method were used for the approximation model. The crowding distance in multiobjective particle swarm optimization was selected as the core algorithm. Meanwhile,the max--rain distance algorithm was used for ensuring the accuracy and rationality for trust measure- ment. Thus the results consistent with the real model could be obtained. The optimization results from five groups indicate that the structure mass is decreased at different degrees. The maximum amplitude reduction reaches 14.1 ~. Meanwhile,the first three orders of natural frequencies for the mierosatellite are improved obviously. The successful applications of the approximation model management frame in multi--objective optimization for satellite structure verify the effectiveness and the rationality, which can provide application values for complex engineering multi--objective optimization.

关键词

微小卫星/多目标优化设计/Kriging模型/近似模型管理

Key words

microsatellite/multi -- objective optimization/Kriging model/approximation model management

分类

航空航天

引用本文复制引用

郑侃,廖文和,张翔..基于近似模型管理的微小卫星结构多目标优化设计[J].中国机械工程,2012,23(6):655-659,5.

中国机械工程

OA北大核心CSCDCSTPCD

1004-132X

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