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
Link To Document :
بازگشت