航天控制系统柔性化需求与关键技术分析  

Analysis of flexibility requirements and key technologies for aerospace control systems

作　　者：禹春梅[1] 董文杰[1] 路坤锋[1] 李晓敏[1] 李然 盖一帆 YU Chunmei;DONG Wenjie;LU Kunfeng;LI Xiaomin;LI Ran;GE Yifan(Beijing Aerospace Automatic Control Institute,Beijing 100854,China)

机构地区：[1]北京航天自动控制研究所,北京100854

出　　处：《航天控制》2025年第1期1-7,共7页Aerospace Control

摘　　要：全面剖析了航天控制系统柔性化需求的背景,深入探讨了系统级与单机级所面临的诸多挑战,创新性地提出了“可聚可散、灵活拼装、敏捷定义和弹性互联”的系统级柔性设计理念以及“随形安装、刚柔结合、能屈能伸、柔性操控”的单机级柔性设计理念,阐述了系统软硬件快速组装及互操作管理、多层级通信互联、柔性一体化共形布局与分析、柔性电子的航天环境适应性验证等柔性化的关键技术路径,并在融合创新技术、加强跨领域合作、建立标准规范以及拓展与深化应用等方面对航天控制系统柔性化发展趋势进行了展望。The requirements of the flexibility of aerospace control system are extensively analyzed in this paper,and the challenges are deeply discussed,which are concentrated on the system level and the device level.The design concept of the flexibility of the system level and the device level is proposed in innovation,and the key technical path of the flexibility of the system level and the device level is further elaborated,such as rapid assembly and interoperability management of system software and hardware,multi-level communication interconnection,flexible integrated conformal layout and analysis,and verifi⁃cation of the adaptability of flexible electronics to the aerospace environment,and the development trend of the flexibility of the aerospace control system is finally visioned in terms of integrating innovative tech⁃nologies,strengthening cross domain cooperation,establishing standards and specifications,and expanding and deepening applications.

关 键 词：未来航天器 控制系统 系统级柔性 单机级柔性 柔性电子 

分 类 号：V448.2[航空宇航科学与技术—飞行器设计]