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空间站姿态控制系统实时仿真研究
引用本文:梁为升,徐世杰.空间站姿态控制系统实时仿真研究[J].飞行力学,2004,22(4):25-28.
作者姓名:梁为升  徐世杰
作者单位:北京航空航天大学,宇航学院,北京,100083
摘    要:研究了五棱锥构型的单框架控制力矩陀螺群作为执行机构的空间站姿态控制系统的实时仿真问题.根据空间站姿态控制系统的实时分布式仿真要求设计了仿真节点结构,综合了四种网络连接形式构建系统的实时网络环境,说明了仿真系统软、硬件平台的选择,以及系统仿真中的调度设计问题.最后对整个系统进行了分布实时仿真,运行结果说明了这种空间站姿态控制系统方案是可行的.

关 键 词:空间站  姿态控制  模型  实时仿真  控制力矩陀螺
文章编号:1002-0853(2004)04-0025-04
修稿时间:2003年10月8日

Study of Real Time Simulation for Attitude Control Systems of a Space Station
LIANG Wei-sheng,XU Shi-jie.Study of Real Time Simulation for Attitude Control Systems of a Space Station[J].Flight Dynamics,2004,22(4):25-28.
Authors:LIANG Wei-sheng  XU Shi-jie
Abstract:This paper studies real time simulation for the attitude control system of a space station which applies SGCMGs with five as actuators.Simulation nodes and structures are designed according to the requirement of the distributed real time simulation. Four kinds of connecting type are used for constructing the real time network. Software and hardware are selected for the simulation system, and the problem about system scheduling is explained. Finally, the distributed real time simulation is realized. The simulating results show that this kind of attitude control systems of the space station is feasible.
Keywords:space station  attitude control  model  real time simulation  control moment gyroscope
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