航天器布局方案设计  

Spacecraft layout design

作　　者：滕弘飞[1] 张宝[1] 刘峻[1] 李广强[1] 孙治国[1] 

机构地区：[1]大连理工大学机械工程学院

出　　处：《大连理工大学学报》2003年第1期86-92,共7页Journal of Dalian University of Technology

基　　金：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).

摘　　要：航天器布局方案设计是研究如何充分利用航天器有限的空间,布置尽可能多的组件或仪器、设备,并满足其内部和周围环境的各种约束要求的问题,是一个多学科交叉课题,其实质是研究大型、高维、动态复杂工程系统方案设计的建模、求解和自动化设计的理论和方法.综述了航天器总体和航天器舱体、气动外形、太阳帆、天线、稳定平台、姿控发动机、复杂插座、电路板等部分组件布局设计,着重从实用化角度出发论述了其设计方法、应用及发展趋势.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.

关 键 词：航天器 布局方案设计 舱体 气动外形 太阳帆 总体设计 

分 类 号：V423[航空宇航科学与技术—飞行器设计]