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航天器控制系统是一种典型的信息-物理融合系统(CPS),应用CPS技术将是提高航天器控制系统设计正确性和效率的一个重要途径.在探讨CPS系统特征和CPS技术研究的进展以及分析航天器控制系统的技术特点的基础上,分析了在航天器控制系统中应用CPS技术的可行性,提出了基于CPS技术的系统设计的新思路和技术途径,并研究了在航天器控制系统中应用CPS技术需解决的问题和面临的挑战.
Spacecraft control system is a typical information-physical fusion system (CPS), and the application of CPS technology will be an important way to improve the accuracy and efficiency of spacecraft control system design.In the study of CPS system features and CPS technology research progress and Based on the analysis of the technical characteristics of the spacecraft control system, the feasibility of applying CPS technology to the spacecraft control system is analyzed. A new idea and technical approach of system design based on CPS technology are proposed. In the spacecraft control system In the application of CPS technology to solve the problems and challenges.