DocumentCode :
1434063
Title :
Air-Gap-Power-Vector-Based Sensorless Method for DFIG Control Without Flux Estimator
Author :
Marques, G.D. ; Sousa, D.M.
Author_Institution :
Dept. of Electr. & Comput. Eng., Tech. Univ. of Lisbon, Lisbon, Portugal
Volume :
58
Issue :
10
fYear :
2011
Firstpage :
4717
Lastpage :
4726
Abstract :
A sensorless method for the direct estimation of the slip position of the wound-rotor induction machine is introduced, discussed, and experimentally validated in this paper. The slip position is necessary for the implementation of control by flux orientation. The method proposed is based on the phase comparison of an estimated air-gap power vector and the measured rotor currents in a common reference frame. The proposed method can be implemented in the rotor or in the field reference frames with a hysteresis or proportional-integral controller. The method is sensitive to the stator no-load active and reactive powers, but this dependence is not very important. Simulation and experimental results show that the method is appropriate for the vector control of the doubly fed induction machine. Unlike other methods, this method gives acceptable results when the load is small. In addition, it does not need a flux estimator for the implementation of flux orientation.
Keywords :
PI control; asynchronous machines; hysteresis; machine vector control; magnetic flux; reactive power; rotors; sensorless machine control; stators; DFIG control; air gap power vector-based sensorless method; direct estimation; doubly fed induction machine; flux orientation; hysteresis controller; proportional integral controller; reactive power; slip position estimation; stator no-load active power; wound rotor induction machine; Current measurement; Hysteresis; Induction generators; Sensorless control; Doubly fed induction generator (DFIG); induction generator; sensorless;
fLanguage :
English
Journal_Title :
Industrial Electronics, IEEE Transactions on
Publisher :
ieee
ISSN :
0278-0046
Type :
jour
DOI :
10.1109/TIE.2011.2107716
Filename :
5699919
Link To Document :
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