DocumentCode
1221157
Title
A Virtual Instrument for the Testing and Performance Evaluation of a Microsatellite Power Supply System
Author
Zheng, Chao ; Low, Kay-Soon
Author_Institution
Sch. of Electr. & Electron. Eng., Nanyang Technol. Univ., Singapore
Volume
57
Issue
8
fYear
2008
Firstpage
1808
Lastpage
1815
Abstract
A multimission microsatellite is currently being built by the Satellite Engineering Centre, Nanyang Technological University, Singapore, in collaboration with the DSO National Laboratories, Singapore. Among the various subsystems, the power supply is one of the most critical parts of the satellite. Its primary and secondary power sources, i.e., the solar array and the battery, and the various power converters are responsible for supplying power with well-regulated voltages to the satellite throughout the whole mission. To test and evaluate the performance of the system, with the satellite operating in different simulated space scenarios, a virtual-instrument-based test and measurement system has been developed. Experimental results that were obtained from the setup have shown that the system is a valuable tool that provides data that are difficult to obtain from analysis and software simulation.
Keywords
artificial satellites; space vehicle power plants; DSO National Laboratories; Nanyang Technological University; Satellite Engineering Centre; microsatellite power supply system; multimission microsatellite; primary power sources; secondary power sources; virtual instrument; virtual-instrument-based measurement system; virtual-instrument-based test; Battery; microsatellite; modeling; power supply system (PSS); virtual instrument (VI);
fLanguage
English
Journal_Title
Instrumentation and Measurement, IEEE Transactions on
Publisher
ieee
ISSN
0018-9456
Type
jour
DOI
10.1109/TIM.2008.923772
Filename
4523344
Link To Document