Lab VIEW based Implementation of Remedial Action for DC Arcing Faults in a Spacecraft

James A. Momoh, D. M.V. Kumar, Ayodele S. Ishola-Salawu, R. Sowah, Robert Button

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

7 Citations (Scopus)

Abstract

In this paper remedial action for DC arcing faults in spacecraft has been designed and implemented using Lab VIEW. The Lab VIEW is an innovative graphical programming system designed to facilitate computer controlled data acquisition and analysis. DC arcing faults in spacecraft has been designed and implemented using the experimental data obtained at NASA Glenn research center. It is important to keep the continuity of the power supply and at the same time increase the reliability of spacecraft energy power system. In the frequency domain, Fast Fourier Transformation (FFT) is used for the feature extraction of the fault signal and odd harmonics frequency components of the phase currents are analyzed.

Original languageEnglish
Title of host publication2003 IEEE Power Engineering Society General Meeting, Conference Proceedings
Pages491-498
Number of pages8
Publication statusPublished - 2003
Externally publishedYes
Event2003 IEEE Power Engineering Society General Meeting - Toronto, Ont.
Duration: 13 Jul 200317 Jul 2003

Publication series

Name2003 IEEE Power Engineering Society General Meeting, Conference Proceedings
Volume1

Conference

Conference2003 IEEE Power Engineering Society General Meeting
Country/TerritoryCanada
CityToronto, Ont.
Period13/07/0317/07/03

Keywords

  • DC Arcing faults
  • Implementation
  • Lab VIEW
  • Spacecraft

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