Active Disturbance Rejection Control for Air-Breathing Hypersonic Vehicles Based on Prescribed Performance Function

Aiming at the longitudinal motion model of the air-breathing hypersonic vehicles (AHVs) with parameter uncertainties, a new prescribed performance-based active disturbance rejection control (PP-ADRC) method was proposed. First, the AHV model was divided into a velocity subsystem and altitude system....

Full description

Bibliographic Details
Main Authors: Chenyang Xu, Humin Lei, Na Lu
Format: Article
Language:English
Published: Hindawi Limited 2019-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2019/4129136
id doaj-ad633e6dc141431aae8d9c6fbb30dd32
record_format Article
spelling doaj-ad633e6dc141431aae8d9c6fbb30dd322020-11-25T02:04:08ZengHindawi LimitedInternational Journal of Aerospace Engineering1687-59661687-59742019-01-01201910.1155/2019/41291364129136Active Disturbance Rejection Control for Air-Breathing Hypersonic Vehicles Based on Prescribed Performance FunctionChenyang Xu0Humin Lei1Na Lu2Air and Missile Defense College, Air Force Engineering University, Xi’an 710051, ChinaAir and Missile Defense College, Air Force Engineering University, Xi’an 710051, ChinaUnit 93142, People’s Liberation Army, Chengdu 610044, ChinaAiming at the longitudinal motion model of the air-breathing hypersonic vehicles (AHVs) with parameter uncertainties, a new prescribed performance-based active disturbance rejection control (PP-ADRC) method was proposed. First, the AHV model was divided into a velocity subsystem and altitude system. To guarantee the reliability of the control law, the design process was based on the nonaffine form of the AHV model. Unlike the traditional prescribed performance control (PPC), which requires accurate initial tracking errors, by designing a new performance function that does not depend on the initial tracking error and can ensure the small overshoot convergence of the tracking error, the error convergence process can meet the desired dynamic and steady-state performance. Moreover, the designed controller combined with an active disturbance rejection control (ADRC) and extended state observer (ESO) further enhanced the disturbance rejection capability and robustness of the method. To avoid the differential expansion problem and effectively filter out the effects of input noise in the differential signals, a new tracking differentiator was proposed. Finally, the effectiveness of the proposed method was verified by comparative simulations.http://dx.doi.org/10.1155/2019/4129136
collection DOAJ
language English
format Article
sources DOAJ
author Chenyang Xu
Humin Lei
Na Lu
spellingShingle Chenyang Xu
Humin Lei
Na Lu
Active Disturbance Rejection Control for Air-Breathing Hypersonic Vehicles Based on Prescribed Performance Function
International Journal of Aerospace Engineering
author_facet Chenyang Xu
Humin Lei
Na Lu
author_sort Chenyang Xu
title Active Disturbance Rejection Control for Air-Breathing Hypersonic Vehicles Based on Prescribed Performance Function
title_short Active Disturbance Rejection Control for Air-Breathing Hypersonic Vehicles Based on Prescribed Performance Function
title_full Active Disturbance Rejection Control for Air-Breathing Hypersonic Vehicles Based on Prescribed Performance Function
title_fullStr Active Disturbance Rejection Control for Air-Breathing Hypersonic Vehicles Based on Prescribed Performance Function
title_full_unstemmed Active Disturbance Rejection Control for Air-Breathing Hypersonic Vehicles Based on Prescribed Performance Function
title_sort active disturbance rejection control for air-breathing hypersonic vehicles based on prescribed performance function
publisher Hindawi Limited
series International Journal of Aerospace Engineering
issn 1687-5966
1687-5974
publishDate 2019-01-01
description Aiming at the longitudinal motion model of the air-breathing hypersonic vehicles (AHVs) with parameter uncertainties, a new prescribed performance-based active disturbance rejection control (PP-ADRC) method was proposed. First, the AHV model was divided into a velocity subsystem and altitude system. To guarantee the reliability of the control law, the design process was based on the nonaffine form of the AHV model. Unlike the traditional prescribed performance control (PPC), which requires accurate initial tracking errors, by designing a new performance function that does not depend on the initial tracking error and can ensure the small overshoot convergence of the tracking error, the error convergence process can meet the desired dynamic and steady-state performance. Moreover, the designed controller combined with an active disturbance rejection control (ADRC) and extended state observer (ESO) further enhanced the disturbance rejection capability and robustness of the method. To avoid the differential expansion problem and effectively filter out the effects of input noise in the differential signals, a new tracking differentiator was proposed. Finally, the effectiveness of the proposed method was verified by comparative simulations.
url http://dx.doi.org/10.1155/2019/4129136
work_keys_str_mv AT chenyangxu activedisturbancerejectioncontrolforairbreathinghypersonicvehiclesbasedonprescribedperformancefunction
AT huminlei activedisturbancerejectioncontrolforairbreathinghypersonicvehiclesbasedonprescribedperformancefunction
AT nalu activedisturbancerejectioncontrolforairbreathinghypersonicvehiclesbasedonprescribedperformancefunction
_version_ 1724944431299166208