DocumentCode
696236
Title
Performance specifications and analysis of a variable speed synchronous generator with a diode rectifier for the All Electric aircraft using the H∞ control approach
Author
Sautreuil, M. ; Sename, O. ; Riu, D. ; Retiere, N.
Author_Institution
Grenoble Electr. Eng. Lab. (G2ELab), Grenoble, France
fYear
2009
fDate
23-26 Aug. 2009
Firstpage
2917
Lastpage
2922
Abstract
This paper deals with the modeling and control of an electrical source for the future “All Electric” aircraft. It is constituted by a rotor wounded synchronous generator and a diode rectifier feeding the DC power system. Using H∞ control theory, this paper shows that usual disturbance rejection standards can not be met with such an electrical power source and new standards should be defined. Simulations on an exact nonlinear model of the power source are used for control validation.
Keywords
DC generators; H∞ control; aircraft; diodes; machine control; rectifiers; synchronous generators; DC power system; H∞ control approach; all electric aircraft; diode rectifier; disturbance rejection standards; rotor wounded synchronous generator; variable speed synchronous generator; Decision support systems; Europe; Liquefied natural gas; Synchronous generators;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (ECC), 2009 European
Conference_Location
Budapest
Print_ISBN
978-3-9524173-9-3
Type
conf
Filename
7074851
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