DocumentCode
1229789
Title
Analysis of Aerospace Electric Power System Dynamics with a Digital Computer
Author
Stineman, R.W. ; Voss, J.M. ; King, W.S.
Author_Institution
IEEE, The Boeing Company Seattle, Washington
Volume
2
Issue
2
fYear
1964
fDate
4/1/1964 12:00:00 AM
Firstpage
630
Lastpage
641
Abstract
A mathematical representation of a typical aerospace electric generation system is developed for solution using a digital rather than analog computer. The system consists of a gas turbine driving an electric generator and hydraulic pump. The representation of the speed, voltage, and temperature control loops is detailed. Of importance is the development of a format necessary for digital solution, and of a representation for transient power flow between the exciter and generator field in a brushless generator.
Keywords
Aerodynamics; Analog computers; Generators; Hydraulic turbines; Load flow; Power generation; Power system analysis computing; Power system dynamics; Power system transients; Temperature control;
fLanguage
English
Journal_Title
Aerospace, IEEE Transactions on
Publisher
ieee
ISSN
0536-1516
Type
jour
DOI
10.1109/TA.1964.4319647
Filename
4319647
Link To Document