A Novel Robust Model Predictive Controller for Aerospace Three-Phase PWM Rectifiers

This paper presents a novel Model Predictive Direct Power Control (MPDPC) approach for the pulse width modulation (PWM) rectifiers in the Aircraft Alternating Current Variable Frequency (ACVF) power system. The control performance of rectifiers may be largely affected by variations in the AC side im...

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Main Authors: Tao Lei, Weiwei Tan, Guangsi Chen, Delin Kong
Format: Article
Language:English
Published: MDPI AG 2018-09-01
Series:Energies
Subjects:
Online Access:http://www.mdpi.com/1996-1073/11/9/2490
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spelling doaj-1fab437dacb44b608e54f780bc62a8352020-11-25T01:13:33ZengMDPI AGEnergies1996-10732018-09-01119249010.3390/en11092490en11092490A Novel Robust Model Predictive Controller for Aerospace Three-Phase PWM RectifiersTao Lei0Weiwei Tan1Guangsi Chen2Delin Kong3Key laboratory of Aircraft Electric Propulsion Technology, Ministry of Industry and Information Technology of China, Northwestern Polytechnic University, Xi’an 710072, ChinaKey laboratory of Aircraft Electric Propulsion Technology, Ministry of Industry and Information Technology of China, Northwestern Polytechnic University, Xi’an 710072, ChinaKey laboratory of Aircraft Electric Propulsion Technology, Ministry of Industry and Information Technology of China, Northwestern Polytechnic University, Xi’an 710072, ChinaKey laboratory of Aircraft Electric Propulsion Technology, Ministry of Industry and Information Technology of China, Northwestern Polytechnic University, Xi’an 710072, ChinaThis paper presents a novel Model Predictive Direct Power Control (MPDPC) approach for the pulse width modulation (PWM) rectifiers in the Aircraft Alternating Current Variable Frequency (ACVF) power system. The control performance of rectifiers may be largely affected by variations in the AC side impedance, especially for systems with limited power volume system. A novel idea for estimating the impedance variation based on the Bayesian estimation, using an algorithm embedded in MPDPC is presented in this paper. The input filter inductance and its equivalent series resistance (ESR) of PWM rectifiers are estimated in this algorithm by measuring the input current and input voltage in each cycle with the probability Bayesian estimation theory. This novel estimation method can overcome the shortcomings of traditional data based estimation methods such as least square estimation (LSE), which achieves poor estimation results with the small samples data set. In ACVF systems, the effect on the parameters estimation accuracy caused by the number of sampling points in one cycle is also analyzed in detail by simulation. The validity of this method is verified by the digital and Hard-in-loop simulation compared with other estimation methods such as the least square estimation method. The experimental testing results show that the proposed estimation algorithm can improve the robustness and the control performance of the MPDPC under the condition of the uncertainty of the AC side parameters of the three-phase PWM rectifiers in aircraft electrical power system.http://www.mdpi.com/1996-1073/11/9/2490Model Predictive Direct Power Control (MPDPC)Aircraft Electrical Power SystemPWM rectifiersBayesian estimation methods
collection DOAJ
language English
format Article
sources DOAJ
author Tao Lei
Weiwei Tan
Guangsi Chen
Delin Kong
spellingShingle Tao Lei
Weiwei Tan
Guangsi Chen
Delin Kong
A Novel Robust Model Predictive Controller for Aerospace Three-Phase PWM Rectifiers
Energies
Model Predictive Direct Power Control (MPDPC)
Aircraft Electrical Power System
PWM rectifiers
Bayesian estimation methods
author_facet Tao Lei
Weiwei Tan
Guangsi Chen
Delin Kong
author_sort Tao Lei
title A Novel Robust Model Predictive Controller for Aerospace Three-Phase PWM Rectifiers
title_short A Novel Robust Model Predictive Controller for Aerospace Three-Phase PWM Rectifiers
title_full A Novel Robust Model Predictive Controller for Aerospace Three-Phase PWM Rectifiers
title_fullStr A Novel Robust Model Predictive Controller for Aerospace Three-Phase PWM Rectifiers
title_full_unstemmed A Novel Robust Model Predictive Controller for Aerospace Three-Phase PWM Rectifiers
title_sort novel robust model predictive controller for aerospace three-phase pwm rectifiers
publisher MDPI AG
series Energies
issn 1996-1073
publishDate 2018-09-01
description This paper presents a novel Model Predictive Direct Power Control (MPDPC) approach for the pulse width modulation (PWM) rectifiers in the Aircraft Alternating Current Variable Frequency (ACVF) power system. The control performance of rectifiers may be largely affected by variations in the AC side impedance, especially for systems with limited power volume system. A novel idea for estimating the impedance variation based on the Bayesian estimation, using an algorithm embedded in MPDPC is presented in this paper. The input filter inductance and its equivalent series resistance (ESR) of PWM rectifiers are estimated in this algorithm by measuring the input current and input voltage in each cycle with the probability Bayesian estimation theory. This novel estimation method can overcome the shortcomings of traditional data based estimation methods such as least square estimation (LSE), which achieves poor estimation results with the small samples data set. In ACVF systems, the effect on the parameters estimation accuracy caused by the number of sampling points in one cycle is also analyzed in detail by simulation. The validity of this method is verified by the digital and Hard-in-loop simulation compared with other estimation methods such as the least square estimation method. The experimental testing results show that the proposed estimation algorithm can improve the robustness and the control performance of the MPDPC under the condition of the uncertainty of the AC side parameters of the three-phase PWM rectifiers in aircraft electrical power system.
topic Model Predictive Direct Power Control (MPDPC)
Aircraft Electrical Power System
PWM rectifiers
Bayesian estimation methods
url http://www.mdpi.com/1996-1073/11/9/2490
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