TY - GEN
T1 - Development of fast test platform for microsatellite
AU - Peng, Yu
AU - Liu, Datong
AU - Peng, Xiyuan
AU - Shao, Yunfeng
PY - 2009
Y1 - 2009
N2 - 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.
AB - 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.
KW - Distributed system
KW - Fast test
KW - Microsatellites test
KW - Parallel test
KW - Synthetic instruments
UR - https://www.scopus.com/pages/publications/72249105068
U2 - 10.1109/AUTEST.2009.5314040
DO - 10.1109/AUTEST.2009.5314040
M3 - 会议稿件
AN - SCOPUS:72249105068
SN - 9781424449811
T3 - AUTOTESTCON (Proceedings)
SP - 206
EP - 209
BT - IEEE AUTOTESTCON 2009 Proceedings
T2 - IEEE AUTOTESTCON 2009 - Systems Readiness Technology Conference: Mission Assurance Through Advanced ATE
Y2 - 14 September 2009 through 17 September 2009
ER -