微卫星快速测试平台的研制

Pengpeng Yu, Datong Liu, Xiyuan Peng, Shao Yunfeng
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引用次数: 2

摘要

微卫星是一种用于各种科学研究的空间平台。因此,在其设计、仿真和测试过程中,需要监测和分析的状态和信号非常复杂。根据这些实际需求,针对不同的研究目的,需要考虑适合快速测试的开放式测试平台。因此,本文提出了一种基于SOPC(可编程芯片系统)技术和合成仪器的全新解决方案。采用分布式并行测试体系结构,采用标准高速串行总线LVDS (Low Voltage Differential Signal)作为数据通信和系统控制接口。该测试平台框架开放,扩展性强,具有实时处理微卫星测试的能力。该方法已成功应用于某微卫星试验与仿真系统中,并实现了200ms周期实时监测与测试。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Development of fast test platform for microsatellite
Microsatellite is a kind of platform in space for various scientific researches. So, during its design, simulation and test process, the status and signals should be monitored and analyzed are complicated. According to those kinds of practical requirement, an open test platform suitable for fast test aimed in different research purpose should be considered. Thus, a brand-new solution based on SOPC (System on Programmable Chip) technology and synthetic instruments is presented in this paper. It adopts a distributed parallel test architecture with a standard high speed serial bus LVDS (Low Voltage Differential Signal) as the data communication and system control interface. This test platform has an open framework, a strong expansibility and a real-time processing ability for microsatellites test. It has been successfully applied and implements 200ms periodical real-time monitoring and testing in a microsatellite test and simulation system.
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