DocumentCode :
2567357
Title :
Lab VIEW based implementation of remedial action for DC arcing faults in a spacecraft
Author :
Momoh, James A. ; Kumar, D.M.V. ; Ishola-Salawu, Ayodele S. ; Sowah, R. ; Button, Robert
Author_Institution :
Dept. of Electr. Eng., Howard Univ., Washington, DC, USA
Volume :
1
fYear :
2003
fDate :
13-17 July 2003
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.
Keywords :
aircraft power systems; arcs (electric); data acquisition; data analysis; fast Fourier transforms; feature extraction; power engineering computing; power system faults; power system reliability; DC arcing faults; Lab VIEW; arcing fault detection algorithm; back propagation; computer controlled data acquisition; data analysis; fast Fourier transformation; feature extraction; graphical programming system; harmonic frequency components; phase currents; power supply; reliability; remedial action; spacecraft energy power system; Control systems; Data acquisition; Data analysis; NASA; Power supplies; Power system analysis computing; Power system faults; Power system harmonics; Power system reliability; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Power Engineering Society General Meeting, 2003, IEEE
Print_ISBN :
0-7803-7989-6
Type :
conf
DOI :
10.1109/PES.2003.1267226
Filename :
1267226
Link To Document :
بازگشت