Indirect Vector Control of Linear Induction Motors Using Space Vector Pulse Width Modulation

被引:1
|
作者
Khaliq, Arjmand [1 ]
Kashif, Syed Abdul Rahman [1 ]
Ahmad, Fahad [2 ]
Anwar, Muhammad [3 ]
Shaheen, Qaisar [4 ]
Akhtar, Rizwan [5 ]
Shah, Muhammad Arif [5 ]
Abdelmaboud, Abdelzahir [6 ]
机构
[1] Univ Engn & Technol, Elect Engn Dept, Lahore 54700, Pakistan
[2] Jouf Univ, Dept Basic Sci, Deanship Common Year 1, Sakaka 72341, Aljouf, Saudi Arabia
[3] Univ Educ, Dept Informat Sci, Div Sci & Technol, Lahore 54000, Pakistan
[4] Islamia Univ Bahawalpur, Dept Comp Sci & Informat Technol, Rahim Yar Khan Sub Campus, Rahim Yar Khan, Pakistan
[5] Pak Austria Fachhsch Inst Appl Sci & Technol, Dept IT & Comp Sci, Haripur, Pakistan
[6] King Khalid Univ, Dept Informat Syst, Muhayel Aseer 61913, Saudi Arabia
来源
CMC-COMPUTERS MATERIALS & CONTINUA | 2023年 / 74卷 / 03期
关键词
Space vector pulse width modulation; linear induction motor; proportional-integral controller; indirect vector control; electromechanical dynamic modeling;
D O I
10.32604/cmc.2023.033027
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Vector control schemes have recently been used to drive linear induction motors (LIM) in high-performance applications. This trend pro-motes the development of precise and efficient control schemes for individual motors. This research aims to present a novel framework for speed and thrust force control of LIM using space vector pulse width modulation (SVPWM) inverters. The framework under consideration is developed in four stages. To begin, MATLAB Simulink was used to develop a detailed mathematical and electromechanical dynamic model. The research presents a modified SVPWM inverter control scheme. By tuning the proportional-integral (PI) controller with a transfer function, optimized values for the PI controller are derived. All the subsystems mentioned above are integrated to create a robust simulation of the LIM's precise speed and thrust force control scheme. The reference speed values were chosen to evaluate the performance of the respective system, and the developed system's response was verified using various data sets. For the low-speed range, a reference value of 10 m/s is used, while a reference value of 100 m/s is used for the high-speed range. The speed output response indicates that the motor reached reference speed in a matter of seconds, as the delay time is between 8 and 10 s. The maximum amplitude of thrust achieved is less than 400 N, demonstrating the controller's capability to control a high-speed LIM with minimal thrust ripple. Due to the controlled speed range, the developed system is highly recommended for low-speed and high-speed and heavy-duty traction applications.
引用
收藏
页码:6263 / 6287
页数:25
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