Adaptive hypersonic flight control under asymmetric AOA constraint

Yuyan Guo; Bin Xu; Yueping Wang; Xiaoxiang Hu; Hao Feng; Yonghua Fan

doi:10.23919/ChiCC.2019.8866681

Adaptive hypersonic flight control under asymmetric AOA constraint

Yuyan Guo, Bin Xu, Yueping Wang, Xiaoxiang Hu, Hao Feng, Yonghua Fan

School of Automation

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

This paper investigates an asymmetric barrier Lyapunov function (ABLF) based adaptive learning controller for hypersonic flight vehicle (HFV). With consideration of the asymmetric constraint on angle of attack (AOA), by analysing the ABLF, the controller is designed based on back-stepping technique with AOA constraint being applied. Moreover, the composite learning method is utilized to estimate unknown nonlinear functions. Simulation results verify that the designed controller can guarantee good tracking performance, and the AOA tracking error is well restricted.

Original language	English
Title of host publication	Proceedings of the 38th Chinese Control Conference, CCC 2019
Editors	Minyue Fu, Jian Sun
Publisher	IEEE Computer Society
Pages	8271-8276
Number of pages	6
ISBN (Electronic)	9789881563972
DOIs	https://doi.org/10.23919/ChiCC.2019.8866681
State	Published - Jul 2019
Event	38th Chinese Control Conference, CCC 2019 - Guangzhou, China Duration: 27 Jul 2019 → 30 Jul 2019

Publication series

Name	Chinese Control Conference, CCC
Volume	2019-July
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	38th Chinese Control Conference, CCC 2019
Country/Territory	China
City	Guangzhou
Period	27/07/19 → 30/07/19

Keywords

Angleofattack(AOA)constraint
AsymmetricbarrierLyapunovfunction(ABLF)
Composite learning
Hypersonicflightvehicle(HFV)
Neural networks (NNs)

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10.23919/ChiCC.2019.8866681

Cite this

@inproceedings{5f2adcff9bb84eb8ab08b3dd3f2d3e00,

title = "Adaptive hypersonic flight control under asymmetric AOA constraint",

abstract = "This paper investigates an asymmetric barrier Lyapunov function (ABLF) based adaptive learning controller for hypersonic flight vehicle (HFV). With consideration of the asymmetric constraint on angle of attack (AOA), by analysing the ABLF, the controller is designed based on back-stepping technique with AOA constraint being applied. Moreover, the composite learning method is utilized to estimate unknown nonlinear functions. Simulation results verify that the designed controller can guarantee good tracking performance, and the AOA tracking error is well restricted.",

keywords = "Angleofattack(AOA)constraint, AsymmetricbarrierLyapunovfunction(ABLF), Composite learning, Hypersonicflightvehicle(HFV), Neural networks (NNs)",

author = "Yuyan Guo and Bin Xu and Yueping Wang and Xiaoxiang Hu and Hao Feng and Yonghua Fan",

note = "Publisher Copyright: {\textcopyright} 2019 Technical Committee on Control Theory, Chinese Association of Automation.; 38th Chinese Control Conference, CCC 2019 ; Conference date: 27-07-2019 Through 30-07-2019",

year = "2019",

month = jul,

doi = "10.23919/ChiCC.2019.8866681",

language = "英语",

series = "Chinese Control Conference, CCC",

publisher = "IEEE Computer Society",

pages = "8271--8276",

editor = "Minyue Fu and Jian Sun",

booktitle = "Proceedings of the 38th Chinese Control Conference, CCC 2019",

}

Guo, Y, Xu, B, Wang, Y, Hu, X, Feng, H & Fan, Y 2019, Adaptive hypersonic flight control under asymmetric AOA constraint. in M Fu & J Sun (eds), Proceedings of the 38th Chinese Control Conference, CCC 2019., 8866681, Chinese Control Conference, CCC, vol. 2019-July, IEEE Computer Society, pp. 8271-8276, 38th Chinese Control Conference, CCC 2019, Guangzhou, China, 27/07/19. https://doi.org/10.23919/ChiCC.2019.8866681

Adaptive hypersonic flight control under asymmetric AOA constraint. / Guo, Yuyan; Xu, Bin; Wang, Yueping et al.
Proceedings of the 38th Chinese Control Conference, CCC 2019. ed. / Minyue Fu; Jian Sun. IEEE Computer Society, 2019. p. 8271-8276 8866681 (Chinese Control Conference, CCC; Vol. 2019-July).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Adaptive hypersonic flight control under asymmetric AOA constraint

AU - Guo, Yuyan

AU - Xu, Bin

AU - Wang, Yueping

AU - Hu, Xiaoxiang

AU - Feng, Hao

AU - Fan, Yonghua

PY - 2019/7

Y1 - 2019/7

N2 - This paper investigates an asymmetric barrier Lyapunov function (ABLF) based adaptive learning controller for hypersonic flight vehicle (HFV). With consideration of the asymmetric constraint on angle of attack (AOA), by analysing the ABLF, the controller is designed based on back-stepping technique with AOA constraint being applied. Moreover, the composite learning method is utilized to estimate unknown nonlinear functions. Simulation results verify that the designed controller can guarantee good tracking performance, and the AOA tracking error is well restricted.

AB - This paper investigates an asymmetric barrier Lyapunov function (ABLF) based adaptive learning controller for hypersonic flight vehicle (HFV). With consideration of the asymmetric constraint on angle of attack (AOA), by analysing the ABLF, the controller is designed based on back-stepping technique with AOA constraint being applied. Moreover, the composite learning method is utilized to estimate unknown nonlinear functions. Simulation results verify that the designed controller can guarantee good tracking performance, and the AOA tracking error is well restricted.

KW - Angleofattack(AOA)constraint

KW - AsymmetricbarrierLyapunovfunction(ABLF)

KW - Composite learning

KW - Hypersonicflightvehicle(HFV)

KW - Neural networks (NNs)

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U2 - 10.23919/ChiCC.2019.8866681

DO - 10.23919/ChiCC.2019.8866681

M3 - 会议稿件

AN - SCOPUS:85074393256

T3 - Chinese Control Conference, CCC

SP - 8271

EP - 8276

BT - Proceedings of the 38th Chinese Control Conference, CCC 2019

A2 - Fu, Minyue

A2 - Sun, Jian

PB - IEEE Computer Society

T2 - 38th Chinese Control Conference, CCC 2019

Y2 - 27 July 2019 through 30 July 2019

ER -

Adaptive hypersonic flight control under asymmetric AOA constraint

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Keywords

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