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基于控制总线的内编队控制系统仿真实验设计
引用本文:张斌斌,项军华,刘昆. 基于控制总线的内编队控制系统仿真实验设计[J]. 系统仿真学报, 2012, 24(10): 2087-2090,2097
作者姓名:张斌斌  项军华  刘昆
作者单位:国防科技大学航天与材料工程学院,长沙,410073
摘    要:通过在内编队控制系统仿真实验设计中引入控制总线,实现了从仿真模型建立到模型接入总线的仿真实验,并在仿真实验设计中利用控制总线的特点,设计了总线数据实时符号化显示方案,实现对总线数据的实时监控和符号化显示,完成了对总线数据的实时统计和分析。对内编队卫星稳定工作状态的仿真实验结果表明,基于总线的实时可视化仿真使得对卫星控制系统性能仿真的实验验证过程更加直观高效,为开展内编队卫星控制系统性能仿真和控制方案设计提供了平台。

关 键 词:控制系统  控制总线  内编队卫星  仿真实验

Simulation Experiment Design for Control System in Inner-formation Flying Satellites Based on Control Bus
ZHANG Bin-bin,XIANG Jun-hua,LIU Kun. Simulation Experiment Design for Control System in Inner-formation Flying Satellites Based on Control Bus[J]. Journal of System Simulation, 2012, 24(10): 2087-2090,2097
Authors:ZHANG Bin-bin  XIANG Jun-hua  LIU Kun
Affiliation:(Institute of Aerospace and Material Engineering,National University of Defence Technology,Changsha 410073,China)
Abstract:By introducing control bus into the inner-formation control system,simulation model and its connection to the bus were implemented.Considering the advantages of control bus,a real-time symbolic output solution was designed,which could help to monitor,analyze and show the bus data live.The steady state of the inner-formation flying satellites simulation experiment shows that the visible real-time simulation based on control bus makes control system replication experiment to be much more intuitive and effective.In result,a platform for performance simulation in inner-formation flying control system and control scheme design was provided.
Keywords:control system  control bus  inner-formation flying satellites  simulation experiment
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