摘要
介绍了一套“航天器智能控制实验平台”.它是一套由遥操作计算机和航天器实验装置固连计算机所组成的主、从计算机系统 .航天器实验装置固连计算机基于 VME总线 ,具有很强的 I/O接口能力 ,可以承担复杂航天器实验装置的测控接口任务 .遥操作计算机作为用户操作的终端 .应用所开发的 SIMSAT软件包 ,可以方便地对航天器姿态控制进行多种控制方案的数学仿真和物理实验 .
The sapcecraft intelligental control experimental platform (SICEP) is introduced. It is a master-slave system, which consists of a remote operation computer (ROC) and a spacecraft experimental plant body-linked computer (BLC). Based on the VME bus, BLC has strong I/O interface capacity. So it can meet the measurement and actuation interface requirements of experimental plant of complex spacecraft. The ROC is regarded as user operation terminal. The effectiveness of the SICEP proposed is verified by simulation and experiment results.
出处
《自动化学报》
EI
CSCD
北大核心
2001年第5期695-699,共5页
Acta Automatica Sinica
基金
国防科技"九五"预研重点课题
国家自然科学基金 ( 69984 0 0 7)资助
关键词
航天器
智能控制
实验平台
姿态控制
Computer hardware
Computer simulation
Computer software
Database systems
Intelligent control
Interfaces (computer)
