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空间站运行管理协同设计与决策支持方法研究与应用

Research and Application of Collaborative Design and Decision Support Methods for Space Station Operation and Management

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【作者】 王震; 林西强; 席露华; 蔡正阳; 季逸民; 李英良; 张强;

【Author】 WANG Zhen;LIN Xiqiang;XI Luhua;CAI Zhengyang;JI Yimin;LI Yingliang;ZHANG Qiang;China Manned Space Engineering Office;Technology and Engineering Center for Space Utilization,Chinese Academy of Sciences;School of Management, Hefei University of Technology;Shanghai Institute of Aerospace Systems Engineering;

【通讯作者】 林西强;

【机构】 中国载人航天工程办公室; 中国科学院空间应用工程与技术中心; 合肥工业大学管理学院; 上海宇航系统工程研究所;

【摘要】 中国空间站于2022年底完成在轨建造并全面进入应用与发展阶段。针对空间站长期载人飞行、任务复杂多样及高度动态关联的运行管理需求,结合现有技术手段的不足,提出空间站运行管理协同设计与决策支持方法研究框架。采用基于模型的系统工程方法论,构建多层级闭环的“mV”模型体系,集成流程模型、数据模型、协同设计模型与决策支持模型四大核心模块,开发配套软件平台。通过空间站飞行任务规划典型场景验证表明:所提出的空间站运行管理协同设计与决策支持系统设计方法对空间站运行管理任务支撑能力强、效率高,并可以扩展应用至空间站运行管理的全场景实践过程中。

【Abstract】 The on-orbit construction of the China Space Station has been completed by the end of 2022, marking its full marching into the application and development stage. To address the operational management requirements driven by long-term manned Space flight, complex and diverse tasks, and highly dynamic correlations, as well as the limitations of existing technical approaches, a research framework for collaborative design and decision support methods in space station operation management is proposed. A model-based systems engineering(MBSE) approach is adopted to establish a multilevel closed-loop "mV"(multiple-V) model architecture, integrating four core modules: process model, data model, collaborative design model, and decision support model. A supporting software platform is developed concurrently. Validation through a typical flight mission planning scenario demonstrates that the proposed collaborative design and decision support system design method exhibits strong support capabilities and high efficiency for space station operation management tasks. Its applicability is extended to cover all practical scenarios of space station operation management. The innovation lies in the construction of a dynamic closed-loop model architecture that breaks through the limitations of traditional static design methods, providing a scalable digital solution for complex spacecraft operation management.

  • 【文献出处】 宇航学报 ,Journal of Astronautics , 编辑部邮箱 ,2025年10期
  • 【分类号】V476.1;V57
  • 【下载频次】41
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