Hybrid Flatness-Based Control of Dual Star Induction Machine Drive System for More Electrical Aircraft-Reference-Cited by-同舟云学术

Hybrid Flatness-Based Control of Dual Star Induction Machine Drive System for More Electrical Aircraft

Published:2024-01-01 Issue:1 Volume:9 Page:50-62
ISSN:2543-4292
Container-title:Power Electronics and Drives
language:en
Short-container-title:

Author:

Nesri Mokhtar¹^ORCID,Nounou Kamal²,Sifelislam Guedida²,Benkhoris Mohamed Fouad³,Azeddine Houari³

Affiliation:

1. Ecole superieur Ali Chabati , Reghaia Algiers , Algeria

2. Ecole Militaire Polytechnique, LSEE UER-ELT , Bordj El-Bahri Algiers , Algeria

3. IREENA Laboratory Université de Nantes , Nantes , France

Abstract

Abstract This paper develops a precise method control system for tracking control of a power drive system based on a multi-phase machine under motor parameter and load torque variations. By adding a simple feedforward term based on the flatness theory, a conventional flux oriented control (FOC) can be enforced to have a perfect tracking performance under model parameter and load torque variations. Hence, a hybrid flatness-based control (HFBC) technique is applied to the control of a dual star induction machine (DSIM) and compared to a classical vector control strategy regarding tracking behaviour, robustness, and perturbations rejection. Finally, the simulation and experimental results are provided to verify the effectiveness of the proposed HFBC under uncertainties such as motor parameter and load torque variations. Furthermore, an enhancement of the drive system’s control performances is demonstrated by the improvement of the technique of separation of the objectives of tracking and disturbance rejection. The simulation and experimental results are presented, demonstrating the superiority of the HFBC.

Publisher

Walter de Gruyter GmbH

Link

https://www.sciendo.com/pdf/10.2478/pead-2024-0004

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