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《Journal of Dalian University of Technology》 2003-01
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Spacecraft layout design

TENGHong\|fei1,2,ZHANGBao1,LIUJun1,LIGuang\|qiang1,SUNZhi\|guo1( 1.School of Mech. Eng., Dalian Univ. of Technol., Dalian 116024, China;2.Res. Inst. of Comput. Technol., Dalian Univ. of Technol., Dalian 116024, China )  
The main task of spacecraft layout design is to make full use of limited space of spacecraft to arrange as more components and instruments as possible while satisfying behavior constraints among components and surround environment. It is a multidisciplinary subject, and the essence is to study the modeling theory, resolving method and automatic design of complex engineering system with large\|scale, high dimensional and dynamic behavior constraints. From pragmatic point of view, this paper surveys the methods of spacecraft layout design and their applications to the layout design of spacecraft module, shape of aerodynamic layout, solar sail, antenna, stabilized platform, attitude control engine, complex jack panel, printed circuit board, etc. At last the future directions of spacecraft layout design is pointed out.
【Fund】: 国家自然科学基金资助项目(60073036 50175009 50275019);; 教育部博士学科点专项科研基金资助项目(20010141005).
【CateGory Index】: V421
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