DocumentCode
2914842
Title
Virtual Instrument for a Micro-satellite Power Supply System
Author
Low, K.-S. ; Zheng, C.
Author_Institution
Nanyang Technol. Univ., Nanyang
fYear
2007
fDate
1-3 May 2007
Firstpage
1
Lastpage
6
Abstract
A multi-mission micro-satellite is presently being built by the Satellite Engineering Centre, Nanyang Technological University. Among the various sub-systems, the power supply is one of the most critical parts of the satellite. Its primary and secondary power sources, namely the solar array and the battery as well as the various power converters are responsible for supplying the power with well regulated voltages to the satellite throughout the whole mission. To test and measure the performance/reliability 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 obtained from the setup have shown that the system is a valuable tool providing data that is difficult to obtain from analysis and software simulation.
Keywords
artificial satellites; power supplies to apparatus; space vehicle power plants; virtual instrumentation; multimission microsatellite; power converters; power supply system; solar array; virtual instrument; Battery charge measurement; Extraterrestrial measurements; Instruments; Power engineering and energy; Power supplies; Power system reliability; Satellites; Software tools; System testing; Voltage; micro-satellite; power supply system; virtual instrument;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation and Measurement Technology Conference Proceedings, 2007. IMTC 2007. IEEE
Conference_Location
Warsaw
ISSN
1091-5281
Print_ISBN
1-4244-0588-2
Type
conf
DOI
10.1109/IMTC.2007.379406
Filename
4258463
Link To Document