摘要
本文介绍了卫星半物理仿真系统的组成及实时接口方案设计，给出了其硬件设计技术及软件设计技术，提出了采用以太网将各种数据采集计算机及数据处理计算机联在一起的设计方案，并进行了可靠性分析。
This paper concerns with real-time interface techniques in the spacecraft'shardware-in-the-loop simulation system.At first,the constitution of spacecraft's hardware-in-the-loopsimulation system is introduced.Then,the hardware and software design techniques of real-time interfaceare discussed and the design of connecting the data acquisition computers and data handle computers withEthernet is forwarded.Finally, the reliability of spacecraft's hardware-in-the-loop simulation system isstudied.
出处
《系统仿真学报》
CAS
CSCD
1995年第2期31-35,共5页
Journal of System Simulation
关键词
卫星
半物理仿真系统
实时接口
卫星轨道
Spacecraft's hardware-in-the-loop simulation system Real-time interface Hard-ware and software design Network Reliability.
