• 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