DocumentCode :
2556879
Title :
A method to predict time domain steady state ripple and time integrated EMI safety margins in power systems
Author :
Brumbaugh, David L.
Author_Institution :
Defense & Space Group, Boeing Co., Seattle, WA, USA
fYear :
1994
fDate :
22-26 Aug 1994
Firstpage :
37
Lastpage :
41
Abstract :
A method is presented for predicting time domain steady state ripple voltages in aircraft and aerospace power systems. The method utilizes conducted emissions limits and test data from the equipment and subsystems on the power bus, and a frequency domain bus impedance characterization of the power source. The method is also extended to predict an integrated EMI safety margin (EMISM) relative to a given conducted susceptibility voltage. Calculated results are compared to measurements on an integrated system
Keywords :
aircraft; electric potential; electromagnetic compatibility; electromagnetic interference; power system protection; safety; time-domain analysis; aerospace power systems; aircraft power systems; conducted emissions limits; conducted susceptibility voltage; equipment; frequency domain bus impedance; integrated system; measurements; power bus; power source; steady state ripple voltages; subsystems; test data; time domain steady state ripple; time integrated EMI safety margins; Aerospace safety; Aircraft; Electromagnetic interference; Electronic equipment; Frequency domain analysis; Impedance; Power supplies; Power systems; Steady-state; Voltage;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electromagnetic Compatibility, 1994. Symposium Record. Compatibility in the Loop., IEEE International Symposium on
Conference_Location :
Chicago, IL
Print_ISBN :
0-7803-1398-4
Type :
conf
DOI :
10.1109/ISEMC.1994.385688
Filename :
385688
Link To Document :
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