DocumentCode
1485250
Title
Stability of aircraft D-C systems
Author
Thomas, R. E.
Author_Institution
Wright Air Development Center, Wright-Patterson Air Force Base, Ohio
Volume
76
Issue
10
fYear
1957
Firstpage
859
Lastpage
859
Abstract
IT IS IMPORTANT that the aircraft electric power system designer be provided with techniques for evaluating the effects of inverter loads on the stability of d-c systems. Inverter-induced instability has been a problem for a number of years. In the past, the problem has been resolved by arbitrarily changing the time response of some element of the system. Stability criteria have now been developed on the basis of measurable properties of the system.
Keywords
Frequency response; Inverters; Mathematical model; Power system stability; Resonant frequency; Stability criteria;
fLanguage
English
Journal_Title
Electrical Engineering
Publisher
ieee
ISSN
0095-9197
Type
jour
DOI
10.1109/EE.1957.6442751
Filename
6442751
Link To Document