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A Sensorless Heavy Load Starting Control Method For SRMs With Residual Inductance Calculation and Polynomial Fitting
Indexado
WoS WOS:001273016800001
Scopus SCOPUS_ID:85219489498
DOI 10.1109/TIE.2024.3413819
Año 2024
Tipo artículo de investigación

Citas Totales

Autores Afiliación Chile

Instituciones Chile

% Participación
Internacional

Autores
Afiliación Extranjera

Instituciones
Extranjeras


Abstract



In this letter, we propose a novel position sensorless control method for switched reluctance machines (SRMs). This method is based on a residual inductance calculation and a polynomial fitting solution. Due to its ability to implement position sensorless heavy load starting control, the proposed method eliminates the need for filters and additional hardware; Not only numerical information about the inductance of each phase of the motor is used but also information about the shape of the inductance curve. The use of multiple information can improve robustness and overcome errors due to the integral term at low speed, so it enables fast motor starting without the need for a position sensor, even under heavy load conditions up to twice the rated load. Its effectiveness is validated through experimental results. Furthermore, it exhibits reasonable simplicity and robustness; thus, providing a promising solution for implementing position sensorless control in SRMs.

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Disciplinas de Investigación



WOS
Instruments & Instrumentation
Automation & Control Systems
Engineering, Electrical & Electronic
Scopus
Electrical And Electronic Engineering
Control And Systems Engineering
SciELO
Sin Disciplinas

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Publicaciones WoS (Ediciones: ISSHP, ISTP, AHCI, SSCI, SCI), Scopus, SciELO Chile.

Colaboración Institucional



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Autores - Afiliación



Ord. Autor Género Institución - País
1 Ge, Lefei - Northwestern Polytech Univ - China
Jianghuai Adv Technol Ctr - China
Northwestern Polytechnical University - China
Jianghuai Advance Technology Center - China
2 Zhang, Dongpeng - Northwestern Polytech Univ - China
Northwestern Polytechnical University - China
3 Huang, Jiale - Northwestern Polytech Univ - China
Northwestern Polytechnical University - China
4 Liu, Senyi - Tongji Univ - China
Tongji University - China
5 Xiao, Dianxun - Hong Kong Univ Sci & Technol - China
Hong Kong University of Science and Technology - Hong Kong
6 Song, Shoujun - Northwestern Polytech Univ - China
Northwestern Polytechnical University - China
7 RODRIGUEZ-PEREZ, JOSE RAMON Hombre Universidad San Sebastián - Chile

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Financiamiento



Fuente
National Natural Science Foundation of China
Fundamental Research Funds for the Central Universities
Aeronautical Science Foundation of China
Shanxi Provincial Key Research and Development Project
AVIC Shaanxi Aero Electric Co., Ltd
Dreams Foundation of Jianghuai Advance Technology Center
Key Research and Development Program of Shaanxi Province
Shaanxi Provincial Science Foundation for Distinguished Young Scholars

Muestra la fuente de financiamiento declarada en la publicación.

Agradecimientos



Agradecimiento
This work was supported in part by the National Natural Science Foundation of China under Grant 52107055 and Grant 52277067; in part by the Key Research and Development Program of Shaanxi Province under Grant 2022GY-260;in part by the Dreams Foundation of Jianghuai Advance Technology Center under Grant 2023-ZM01J001; in part by the Aeronautical Science Foundation of China under Grant 20220040053001; in part by the Fundamental Research Funds for the Central Universities under Grant D5000230069; in part by the Shaanxi Provincial Science Foundation for Distinguished Young Scholars under Grant 2023-JC-JQ44; and in part by research projects of AVIC Shaanxi Aero Electric Co., Ltd under Grant JSJSHT2312280030.
This work was supported in part by the National Natural Science Foundation of China under Grant 52107055 and Grant 52277067; in part by the Key Research and Development Program of Shaanxi Province under Grant 2022GY-260; in part by the Dreams Foundation of Jianghuai Advance Technology Center under Grant 2023-ZM01J001; in part by the Aeronautical Science Foundation of China under Grant 20220040053001; in part by the Fundamental Research Funds for the Central Universities under Grant D5000230069; in part by the Shaanxi Provincial Science Foundation for Distinguished Young Scholars under Grant 2023- JC-JQ44; and in part by research projects of AVIC Shaanxi Aero Electric Co., Ltd under Grant JSJSHT2312280030.

Muestra la fuente de financiamiento declarada en la publicación.