基于数字化研制模式的卫星总装状态闭环管控研究  

Research of Closed-loop Management of Satellite Integrated Assembly Status Base on Digital R&D Mode

作　　者：袁金如[1] 陈强[1] 姚骏[1] 张栖诚 徐天水 王晓波 Yuan Jinru;Chen Qiang;Yao Jun;Zhang Qicheng;Xu Tianshui;Wang Xiaobo(Shanghai Institute of Satellite Engineering,Shanghai 201109)

机构地区：[1]上海卫星工程研究所,上海201109

出　　处：《航天制造技术》2021年第5期74-78,共5页Aerospace Manufacturing Technology

摘　　要：基于卫星数字化研制总装技术状态管控需求,介绍了卫星总装设计技术状态管理实践和总装制造过程技术状态管控及闭环融合实现方法及初步系统构想,为卫星设计制造一体化技术状态管控与数据融合应用提供借鉴与参考。To control the status of satellite digital design and integrated assembly,a management practice of satellite integrated assembly design is proposed,also with the management,the method of closed-loop fusion and the preliminary system thoughts of integrated assembly.This provides reference for the status management and the record fusion application of satellites design and manufacturing integration.

关 键 词：数字化研制模式 卫星总装 设计制造一体化 技术状态 闭环管控 

分 类 号：V57[航空宇航科学与技术—航空宇航推进理论与工程]