Title :
Virtual Instrument for a Micro-satellite Power Supply System
Author :
Low, K.-S. ; Zheng, C.
Author_Institution :
Nanyang Technol. Univ., Nanyang
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;
Conference_Titel :
Instrumentation and Measurement Technology Conference Proceedings, 2007. IMTC 2007. IEEE
Conference_Location :
Warsaw
Print_ISBN :
1-4244-0588-2
DOI :
10.1109/IMTC.2007.379406