Control of a Hybrid Excitation Synchronous Generator for Aircraft Applications

被引：100

作者：

Patin, Nicolas ^{[1
]}

Vido, Lionel ^{[2
,3
,4
]}

Monmasson, Eric ^{[2
,3
,4
]}

Louis, Jean-Paul ^{[5
]}

Gabsi, Mohamed ^{[3
,4
]}

Lecrivain, Michel ^{[3
,4
,6
]}

机构：

[1] Univ Technol Compiegne, Ctr Rech Royallieu, Electromech Lab, F-60205 Compiegne, France

[2] Univ Cergy Pontoise, F-95011 Cergy Pontoise, France

[3] CNRS, F-75794 Paris, France

[4] Univ Paris Sud, F-91190 St Aubin, France

[5] Ecole Normale Super, CNRS, UMR 8029, SATIE, F-94235 Cachan, France

[6] Conservatoire Natl Arts & Metiers, F-75141 Paris, France

来源：

IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS | 2008年 / 55卷 / 10期

关键词：

Aircraft; brushless structure; control; dc generator; embedded systems; hybrid excitation; synchronous machine;

D O I：

10.1109/TIE.2008.924030

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper deals with the control of a hybrid excitation synchronous generator which is used to supply an isolated grid for aircraft applications. This grid is supposed to be a 270-V dc bus. Thus, a rectifier is required between the machine and the de bus. A diode rectifier is preferred here due to its great reliability and because it is also a low-cost solution. A controller is then proposed in order to regulate the output de voltage of the generator. It is finally validated by simulations and experimental results.

引用

页码：3772 / 3783

页数：12

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