Abstract

A sensorless method for the estimation of the rotor position of the wound-rotor induction machine is described in this paper. The method is based on the MRAS methodology and consists in the comparison of two models for the evaluation of the active power transferred across the air gap: the reference model and the adaptive model. The reference model obtains the power transferred across the air gap using directly available and measured stator variables. The adaptive model obtains the same quantity in function of electromotive forces and rotor currents that are measurable on the rotor position, which is under estimation. The method does not need any information about the stator or rotor flux and can be implemented in the rotor or in the stator reference frames with a hysteresis or with a PI controller. The stability analysis gives an unstable region on the rotor current dq plane. Simulation and experimental results show that the method is appropriate for the vector control of the doubly fed induction machine under the stability region.

Highlights

  • The Doubly fed Induction Generator (DFIG) is very attractive for Adjustable Speed Constant Frequency (ASCF) generators with limited speed range

  • In [3] a sensorless control method based in the control of the angle between a reference frame connected to the stator voltage or flux vector and the rotor current vector, was presented

  • This paper presents a new sensorless algorithm to detect the rotor position based on the Model Reference Adaptive System (MRAS) procedure

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Summary

Introduction

The Doubly fed Induction Generator (DFIG) is very attractive for Adjustable Speed Constant Frequency (ASCF) generators with limited speed range. In [3] a sensorless control method based in the control of the angle between a reference frame connected to the stator voltage or flux vector and the rotor current vector, was presented. This paper presents a new sensorless algorithm to detect the rotor position based on the Model Reference Adaptive System (MRAS) procedure. It is based on the comparison of active power transferred on the air gap computed in two different ways.

Description of the Method
Stability Analysis
Sensibility Analysis
Experimental Results
Conclusions
E M Figure 9
Full Text
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