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航天器平台-载荷-控制一体化协同研制
引用本文:王光远,祖家国,李潇,王腾,洪斌,田景峰.航天器平台-载荷-控制一体化协同研制[J].南京航空航天大学学报,2018,50(S1):123-129.
作者姓名:王光远  祖家国  李潇  王腾  洪斌  田景峰
作者单位:北京空间飞行器总体设计部, 北京, 100094
摘    要:航天器任务能力的指标提升,对卫星系统设计的深入、精细以及集约要求更高。以系统性能最优为终极目标,围绕任务能力开展多学科一体化设计,进而引起的产品集成、验证模式的显著改变。本文对国内外航天器多学科一体化研制模式的发展和应用情况进行介绍,分析了一体化设计的需求和内涵,并对多学科一体化协同平台的实现及探索性应用进行了研究。

关 键 词:一体化协同  多学科  研制模式
收稿时间:2018/3/23 0:00:00
修稿时间:2018/5/30 0:00:00

Integrated Development of Platform, Payload and Control for Spacecraft
WANG Guangyuan,ZU Jiaguo,LI Xiao,WANG Teng,HONG Bin,TIAN Jingfeng.Integrated Development of Platform, Payload and Control for Spacecraft[J].Journal of Nanjing University of Aeronautics & Astronautics,2018,50(S1):123-129.
Authors:WANG Guangyuan  ZU Jiaguo  LI Xiao  WANG Teng  HONG Bin  TIAN Jingfeng
Institution:Beijing Institute of Space System Engineering, Beijing, 100094, China
Abstract:The improvement of the mission capability of spacecraft has made it more demanding for the in-depth, intensive design of satellite system. It is required that the ultimate goal of system performance to be carried out around the mission capability, which in turn will lead to significant changes in product integration and verification models. This paper introduces the development and application of the multi-discipline integrated development model for spacecraft, analyzes the needs and implications of integrated design, and introduces the implementation and exploratory applications of the multidisciplinary integrated collaborative platform.
Keywords:integrated collaborative  multi-disciplinary  development pattern
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