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卫星总体多学科设计优化过程分析 被引量:1

The Analysis on the Multidisciplinary Design Optimization Process for Satellite System
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摘要 多学科设计优化方法是实现卫星设计“快、好、省”目标的有效手段,但在实际应用中存在较大困难。根据多学科设计优化方法中多学科设计、多学科分析和多学科优化问题的分解思路,分析了多学科设计优化方法应用于卫星总体设计存在的现实困难和工程实践中必须考虑的设计因素;通过对卫星总体设计过程的分解与分析,提出了多学科设计优化方法与卫星总体设计流程相融合的技术途径,为进一步构建面向卫星总体设计的分布式协同软件框架提供了参考。 The Multidisciplinary Design Optimization (MIX)) is an effective method to reach the "faster, better, cheaper" goal of satellite design, but it is much difficult for applying MIX) in satellite system engineering. On the basis of the decomposition and coordination principle of multidisciplinary design, multidisciplinary analysis, and multidisciplinary optimization in MIX), it analyzes the actual difficulties in satellite system design process and the design factors involved in satellite engineering practices. A technological solution is proposed to connect MDO methodology with satellite system design flow. The results are helpful to further construct distributed collaborative software framework for satellite system integrated design.
出处 《中国制造业信息化(学术版)》 2006年第8期20-24,共5页
基金 国家自然科学基金资助项目(10302031) 国防基础科研项目(S0300A002-02)
关键词 卫星 总体设计 多学科设计优化 设计因素 设计流程 Satellite System Design Multidisciplinary Design Optimization Design Factors Design Flow
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参考文献7

  • 1胡凌云.多学科设计优化技术在卫星总体设计中的应用[J].中国制造业信息化(学术版),2004,33(1):17-21. 被引量:13
  • 2陈琪峰.飞行器分布式协同进化多学科设计优化方法研究[D].长沙:国防科学技术大学,2003:107-127.
  • 3Cullimore B, Panczak T, Baumann J, et al. Automated Multidisciplinary Optimization of a Space - based Telescope [EB/OL]. http://www, crtech, com/docs/papers/2002/optiOpt -ICES2002b. pdf, 2006-07-04.
  • 4Varatharajoo R, Kahle R, Fasoulas S. Approach for combing spacecraft attitude and thermal control systems [J]. Journal of Spacecraft and Rocket, 2003, 40(5): 657-664.
  • 5Irene A B, John R O. Design and development of a satellite constellation using collaborative optimization [J]. Journal of Spacecraft and Rockets, 2004, 41(6): 956-963.
  • 6James R Wertz, Wiley J Larson. Space Mission Analysis and Design (3rd Edition) [M]. Torrance, California: Microcosm Press, 1999.
  • 7From J, Kramer S, Pohl E. A small satellite system design process [A]. Proceedings of the IEEE 1997 National Aerospace and Electronics Conference[C]. OH, USA: IEEE, 1997: 423-429, CH36015-97/0000-0423.

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同被引文献23

  • 1赵伶丰,王海龙,白光明,刘霞.航天器多学科设计优化技术综述[J].航天器工程,2007,16(5):104-109. 被引量:11
  • 2王书河,何麟书.飞行器多学科设计优化概述[J].宇航学报,2004,25(6):697-701. 被引量:26
  • 3卢天健,何德坪,陈常青,赵长颖,方岱宁,王晓林.超轻多孔金属材料的多功能特性及应用[J].力学进展,2006,36(4):517-535. 被引量:252
  • 4唐辉,侯俊杰.多学科设计优化技术在航天航空领域中的应用[J].军民两用技术与产品,2007(3):3-4. 被引量:2
  • 5AIAA Technical Committee for MDC.On current state art multidisciplinary design optimization,AIAA 91-60531[R].Washington D.C.:AIAA,1991.
  • 6张雷,王栋,金光.轻型空间相机热补偿与结构一体化设计研究[C]//中国空间科学学会空间机电与空间光学专业委员会-空间材料专业委员会联合学术交流会论文集.北京:中国空间科学学会,2009:246-250.
  • 7G T David,Curran,T Tung.Weight optimization for honeycomb radiators with embedded heat pipes[J].Journal of Spacecraft and Rockets,1996,33(6):822-828.
  • 8Williams A D,Underwood R L,Arritt B J.Biologically inspired multifunctional composite panel with integrated thermal control[C]//Proceedings of the 51st AIAA Structures,Structural Dynamics and Materials Conference.Washington D.C.:AIAA,2010:1-11.
  • 9T Douglas,Queheillalt.A multifunctional heat pipe sandwich panel structure[J].International Journal of Heat and Mass Transfer,2008,51(3):312-326.
  • 10Sihn S,Ganguli S,Anderson D P,et al.Enhancement of through thickness thermal conductivity of sandwich construction using carbon foam[J].Composites Science and Technology,2012,72(7):767-773.

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