Spacecraft Flight Control Simulation and Parallel Systems

被引:0
|
作者
Yuan L. [1 ]
Cheng M. [1 ]
Wang L. [1 ]
机构
[1] Beijing Institute of Control Engineering, Beijing
来源
Yuhang Xuebao/Journal of Astronautics | 2021年 / 42卷 / 08期
关键词
Chang'e-5 probe; Decision and support; Ground simulation; Parallel systems; Spacecraft flight control;
D O I
10.3873/j.issn.1000-1328.2021.08.006
中图分类号
学科分类号
摘要
This paper firstly summarizes and analyzes the developing status and requirement of spacecraft flight control simulation and parallel systems. In view of the current generalization and standardization of China's spacecraft flight control simulation and parallel systems, an assemblable definition and system architecture of spacecraft flight control simulation and parallel systems is proposed. Then it elaborates on the design of two-component simulation and verification, decision and support. The validity of the system is verified by the flight control of Chang'e-5. The paper finally gives a prospect of the future direction of spacecraft flight control simulation and parallel systems development. © 2021, Editorial Dept. of JA. All right reserved.
引用
收藏
页码:982 / 988
页数:6
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