Design of an NSMCR Based Controller for All-Electric Aircraft Anti-Skid Braking System
In this paper, a relative threshold event-triggered based novel complementary sliding mode control (NSMCR) algorithm of all-electric aircraft (AEA) anti-skid braking system (ABS) is proposed to guarantee the braking stability and tracking precision of reference wheel slip control. First, a model of...
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MDPI AG
2022-05-01
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Series: | Mathematics |
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Online Access: | https://www.mdpi.com/2227-7390/10/10/1715 |
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author | Xuelin Liang Fengrui Xu Mengqiao Chen Wensheng Liu |
author_facet | Xuelin Liang Fengrui Xu Mengqiao Chen Wensheng Liu |
author_sort | Xuelin Liang |
collection | DOAJ |
description | In this paper, a relative threshold event-triggered based novel complementary sliding mode control (NSMCR) algorithm of all-electric aircraft (AEA) anti-skid braking system (ABS) is proposed to guarantee the braking stability and tracking precision of reference wheel slip control. First, a model of the braking system is established in strict-feedback form. Then a virtual controller with a nonlinear control algorithm is proposed to address the problem of constraint control regarding wheel slip rate with asymptotical stability. Next, a novel approaching law-based complementary sliding mode controller is developed to keep track of braking pressure. Moreover, the robust adaptive law is designed to estimate the uncertainties of the braking systems online to alleviate the chattering problem of the braking pressure controller. Additionally, to reduce the network communication and actuator wear of AEA-ABS, a relative threshold event trigger mechanism is proposed to transmit the output of NSMC in demand. The simulation results under various algorithms regarding three types of runway indicate that the proposed algorithms can improve the performance of braking control. In addition, the hardware-in-the-loop (HIL) experimental results prove that the proposed methods are practical for real-time applications. |
first_indexed | 2024-03-10T03:28:52Z |
format | Article |
id | doaj.art-5093a5d114994c34807e4022d7bd5473 |
institution | Directory Open Access Journal |
issn | 2227-7390 |
language | English |
last_indexed | 2024-03-10T03:28:52Z |
publishDate | 2022-05-01 |
publisher | MDPI AG |
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series | Mathematics |
spelling | doaj.art-5093a5d114994c34807e4022d7bd54732023-11-23T12:01:22ZengMDPI AGMathematics2227-73902022-05-011010171510.3390/math10101715Design of an NSMCR Based Controller for All-Electric Aircraft Anti-Skid Braking SystemXuelin Liang0Fengrui Xu1Mengqiao Chen2Wensheng Liu3School of Automation, Central South University, Changsha 410083, ChinaSchool of Automation, Central South University, Changsha 410083, ChinaLaboratory of Science and Technology on Integrated Logistics Support, College of Intelligence Science and Technology, National University of Defense Technology, Changsha 410083, ChinaAdvanced Research Center, Central South University, Changsha 410083, ChinaIn this paper, a relative threshold event-triggered based novel complementary sliding mode control (NSMCR) algorithm of all-electric aircraft (AEA) anti-skid braking system (ABS) is proposed to guarantee the braking stability and tracking precision of reference wheel slip control. First, a model of the braking system is established in strict-feedback form. Then a virtual controller with a nonlinear control algorithm is proposed to address the problem of constraint control regarding wheel slip rate with asymptotical stability. Next, a novel approaching law-based complementary sliding mode controller is developed to keep track of braking pressure. Moreover, the robust adaptive law is designed to estimate the uncertainties of the braking systems online to alleviate the chattering problem of the braking pressure controller. Additionally, to reduce the network communication and actuator wear of AEA-ABS, a relative threshold event trigger mechanism is proposed to transmit the output of NSMC in demand. The simulation results under various algorithms regarding three types of runway indicate that the proposed algorithms can improve the performance of braking control. In addition, the hardware-in-the-loop (HIL) experimental results prove that the proposed methods are practical for real-time applications.https://www.mdpi.com/2227-7390/10/10/1715adaptive backstepping controlcomplementary sliding mode controlnonlinear controlevent-triggered mechanismaircraft braking system |
spellingShingle | Xuelin Liang Fengrui Xu Mengqiao Chen Wensheng Liu Design of an NSMCR Based Controller for All-Electric Aircraft Anti-Skid Braking System Mathematics adaptive backstepping control complementary sliding mode control nonlinear control event-triggered mechanism aircraft braking system |
title | Design of an NSMCR Based Controller for All-Electric Aircraft Anti-Skid Braking System |
title_full | Design of an NSMCR Based Controller for All-Electric Aircraft Anti-Skid Braking System |
title_fullStr | Design of an NSMCR Based Controller for All-Electric Aircraft Anti-Skid Braking System |
title_full_unstemmed | Design of an NSMCR Based Controller for All-Electric Aircraft Anti-Skid Braking System |
title_short | Design of an NSMCR Based Controller for All-Electric Aircraft Anti-Skid Braking System |
title_sort | design of an nsmcr based controller for all electric aircraft anti skid braking system |
topic | adaptive backstepping control complementary sliding mode control nonlinear control event-triggered mechanism aircraft braking system |
url | https://www.mdpi.com/2227-7390/10/10/1715 |
work_keys_str_mv | AT xuelinliang designofannsmcrbasedcontrollerforallelectricaircraftantiskidbrakingsystem AT fengruixu designofannsmcrbasedcontrollerforallelectricaircraftantiskidbrakingsystem AT mengqiaochen designofannsmcrbasedcontrollerforallelectricaircraftantiskidbrakingsystem AT wenshengliu designofannsmcrbasedcontrollerforallelectricaircraftantiskidbrakingsystem |