Title :
Development of fast test platform for microsatellite
Author :
Yu, Peng ; Liu Datong ; Peng Xiyuan ; Yunfeng, Shao
Author_Institution :
Harbin Inst. of Technol., Harbin, China
Abstract :
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 200 ms periodical real-time monitoring and testing in a microsatellite test and simulation system.
Keywords :
artificial satellites; data communication; system-on-chip; testing; data communication; distributed parallel test architecture; fast test platform; high speed serial bus LVDS; low voltage differential signal; microsatellite; microsatellite monitoring; real-time processing; simulation system; synthetic instruments; system control interface; system on programmable chip technology; test process; Analytical models; Communication standards; Data communication; Instruments; Low voltage; Monitoring; Signal analysis; Signal design; Signal processing; System testing; distributed system; fast test; microsatellites test; parallel test; synthetic instruments;
Conference_Titel :
AUTOTESTCON, 2009 IEEE
Conference_Location :
Anaheim, CA
Print_ISBN :
978-1-4244-4980-4
Electronic_ISBN :
1088-7725
DOI :
10.1109/AUTEST.2009.5314040