国防科技大学学报2011，Vol.35Issue(5)：9-16,8.
分离模块航天器不确定性多学科设计优化
Uncertainty-based Multidisciplinary Design Optimization of Fractionated Modularized Cluster Spacecraft
摘要
Abstract
The Uncertainty-based Multidisciplinary Design Optimization (UMDO) method was studied for the conceptual design of fractionated modularized cluster spacecraft (fractionated spacecraft) , so as to comprehensively assess and optimize life cycle cost, benefit, system robustness and flexibility under uncertainty. Firstly, the UMDO methodology was introduced, as well as the schematic flowchart of UMDO for the fractionated spacecraft conceptual design. Secondly, the system architecture and assessment criteria of the new concept fractionated spacecraft were explained. The disciplinary models, cost models and benefit models were described, and the uncertainties thereof were modeled with probability theory. Thirdly, a notional earth observatory fractionated spacecraft was used as an example to demonstrate the application of UMDO in the fractionated spacecraft conceptual design. The UMDO problem formulation and UMDO procedure organization were presented in detail. The results show that the mean of the net revenue and its robustness under uncertainty can be greatly improved, which verified the effectiveness of UMDO method for fractionated spacecraft conceptual design.关键词
分离模块航天器/不确定性/不确定性多学科设计优化Key words
fractionated modularized cluster spacecraft/ uncertainty/ Uncertainty-based Multidisciplinary Design Optimization (UMDO)分类
航空航天引用本文复制引用
姚雯,陈小前,黄奕勇,Michel van Tooren..分离模块航天器不确定性多学科设计优化[J].国防科技大学学报,2011,35(5):9-16,8.基金项目
国家自然科学基金资助项目(50975280,61004094) （50975280,61004094）
教育部新世纪优秀人才支持计划资助项目(NCET-08-0149) （NCET-08-0149）
国防科技大学优秀研究生创新资助项目(B090102) （B090102）
湖南省研究生科研创新资助项目 （）
