概念设计集成系统与星座方案探索

郭爱斌; 米洁; 董晓琴; 邓家禔

概念设计集成系统与星座方案探索

北京航空航天大学机械工程及自动化学院, 北京 100083

详细信息

作者简介:
郭爱斌(1977- ),男,山西榆次人,博士生,abguo@buaa.edu.cn.

中图分类号: V 457; TP 391.72
计量
- 文章访问数: 5134
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- 被引次数: 20
出版历程
- 收稿日期: 2006-07-10
- 网络出版日期: 2007-05-31

Concept design integrated system and constellation architecture exploration

School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

摘要

摘要: 进一步研究了快速方案选择和概念设计新方法.结合概念设计过程,给出星座方案选择和卫星概念设计的基本模型,在方案探索和概念设计中集成了风险和不确定性分析;应用系统综合设计优化平台(SDOF)开发卫星星座概念设计集成系统,实现卫星星座方案探索优选;集成系统交互、演进、分布式协同设计,可自动运行优化过程,同时可监视和控制设计任务单元运行状况,优化完成后用户可定制设计报告内容和格式;最后介绍了对地观测卫星星座概念设计实例,采用多岛遗传算法进行优化,初步验证了该系统在技术原理上的可行性.
- 卫星设计 /
- 方案选择 /
- 概念设计 /
- 不确定性 /
- SDOF
Abstract: The method of rapid architecture selection and concept design was further discussed. The elementary models of satellite constellation′s architecture selection and concept design combined with concept design process were introduced. Risk and uncertainty analysis were integrated into the models. The integrated system of satellite constellation concept design was realized by using system design optimization framework(SDOF). The design process of the integrated system was given. The satellite constellation architecture selection and concept design proceeded with the interactive, evolving and collaborative fashion. The concept design optimization could be executed automatically, and the operation of design task unit could be monitored and controlled. After the completion of satellite concept design optimization, the design report′s context and style could be tailored by the costumers. The example for the satellite constellation for observing the earth was presented and its optimal result was achieved by using the multi-island genetic algorithm. The result demonstrates the usefulness and validity of the system.
- satellite design /
- architecture selection /
- concept design /
- uncertainty /
- SDOF

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参考文献(1)

[1] Budianto I A, Olds J R. Design and deployment of satellite constellation using collaborative optimization[J]. Journal of Spacecraft and Rockets, 2004, 41(6):956-963 [2] Mcmanus H L, Hastings D E, Warmkesset J M, et al. New methods for rapid architecture selection and conceptual design[J]. Journal of Spacecraft and Rockets,2004,41(1):10-19 [3] 张建明. 机械产品概念设计的若干方法研究 . 大连:大连理工大学机械工程学院,2005 Zhang Jianming. Research on methods for conceptual design of mechanical products . Dalian:School of Mechanical & Engineering, Dalian University of Technology,2005(in Chinese) [4] 曹东兴,檀润华,耿磊,等. 基于功能方法树的机械产品概念设计[J]. 上海交通大学学报,2004,38(6):888-891 Cao Dongxing, Tan Runhua, Geng Lei, et al. Mechanical product conceptual design based on functional means tree[J]．Journal of Shanghai Jiaotong University,2004,38(6):888-891(in Chinese) [5] Jilla C D, Miller D W. Multiobjective, multidisciplinary design optimization methodology for distributed satellite systems[J]. Journal of Spacecraft and Rockets,2004,41(1):39-50 [6] Walton M A, Hastings D E. Application of uncertainty analysis to architecture selection of satellite systems[J].Journal of Spacecraft and Rockets,2004,41(1):75-84 [7] Wertz J R, Larson W J. Space mission analysis and design[M]. 3rd ed. Torrance,CA:Microcosm Press,1999:241-820 [8] Riddle T E. Evaluation of multidisciplonary design optimization techniques as applied to the spacecraft design process . Colorado:Department of Aerospace Engineering Sciences,University of Colorado,1999 [9] 陈琪锋. 飞行器分布式协同进化多学科设计优化方法研究 . 长沙:国防科技大学航天与材料工程学院, 2003 Chen Qifeng. Distributed coevolutionary multidisciplinary design optimization methods for flying vechiles .Changsha:School of Aerospace & Materials Engineering,National University of Defense Technology,2003(in Chinese)

施引文献

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