Hypersonic vehicle longitudinal control based on sliding mode observer and dynamic surface control

Yuyan Guo; Shixing Wang; Bin Xu; Xiaoxiang Hu; Yuan Yuan

doi:10.1109/ChiCC.2016.7555084

Hypersonic vehicle longitudinal control based on sliding mode observer and dynamic surface control

Yuyan Guo, Shixing Wang, Bin Xu, Xiaoxiang Hu, Yuan Yuan

School of Automation

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

4 Scopus citations

Abstract

In this paper, a class of sliding mode observer and a dynamic surface control law are proposed for the longitudinal dynamics of hypersonic flight vehicle. The sliding mode observer is designed to estimate the angle of attack and flight path angle which are usually difficult to measure. Using the estimation results, the back-stepping-based dynamic surface control law is designed to avoid the explosion of complexity caused by continuous integration, and the control method is applied on the hypersonic vehicle longitudinal model to make the aircraft track the reference trajectory precisely. Simulation results have shown that the proposed methods perform well on the control and state estimation of hypersonic vehicle.

Original language	English
Title of host publication	Proceedings of the 35th Chinese Control Conference, CCC 2016
Editors	Jie Chen, Qianchuan Zhao, Jie Chen
Publisher	IEEE Computer Society
Pages	10926-10931
Number of pages	6
ISBN (Electronic)	9789881563910
DOIs	https://doi.org/10.1109/ChiCC.2016.7555084
State	Published - 26 Aug 2016
Event	35th Chinese Control Conference, CCC 2016 - Chengdu, China Duration: 27 Jul 2016 → 29 Jul 2016

Publication series

Name	Chinese Control Conference, CCC
Volume	2016-August
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	35th Chinese Control Conference, CCC 2016
Country/Territory	China
City	Chengdu
Period	27/07/16 → 29/07/16

Keywords

Back-stepping Control
Dynamic Surface Control
Hypersonic Flight Vehicle
Sliding Mode Observer

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10.1109/ChiCC.2016.7555084

Cite this

Guo, Y., Wang, S., Xu, B., Hu, X., & Yuan, Y. (2016). Hypersonic vehicle longitudinal control based on sliding mode observer and dynamic surface control. In J. Chen, Q. Zhao, & J. Chen (Eds.), Proceedings of the 35th Chinese Control Conference, CCC 2016 (pp. 10926-10931). Article 7555084 (Chinese Control Conference, CCC; Vol. 2016-August). IEEE Computer Society. https://doi.org/10.1109/ChiCC.2016.7555084

@inproceedings{946e7a88cace4852b3bd464682e87926,

title = "Hypersonic vehicle longitudinal control based on sliding mode observer and dynamic surface control",

abstract = "In this paper, a class of sliding mode observer and a dynamic surface control law are proposed for the longitudinal dynamics of hypersonic flight vehicle. The sliding mode observer is designed to estimate the angle of attack and flight path angle which are usually difficult to measure. Using the estimation results, the back-stepping-based dynamic surface control law is designed to avoid the explosion of complexity caused by continuous integration, and the control method is applied on the hypersonic vehicle longitudinal model to make the aircraft track the reference trajectory precisely. Simulation results have shown that the proposed methods perform well on the control and state estimation of hypersonic vehicle.",

keywords = "Back-stepping Control, Dynamic Surface Control, Hypersonic Flight Vehicle, Sliding Mode Observer",

author = "Yuyan Guo and Shixing Wang and Bin Xu and Xiaoxiang Hu and Yuan Yuan",

note = "Publisher Copyright: {\textcopyright} 2016 TCCT.; 35th Chinese Control Conference, CCC 2016 ; Conference date: 27-07-2016 Through 29-07-2016",

year = "2016",

month = aug,

day = "26",

doi = "10.1109/ChiCC.2016.7555084",

language = "英语",

series = "Chinese Control Conference, CCC",

publisher = "IEEE Computer Society",

pages = "10926--10931",

editor = "Jie Chen and Qianchuan Zhao and Jie Chen",

booktitle = "Proceedings of the 35th Chinese Control Conference, CCC 2016",

}

Guo, Y, Wang, S, Xu, B, Hu, X & Yuan, Y 2016, Hypersonic vehicle longitudinal control based on sliding mode observer and dynamic surface control. in J Chen, Q Zhao & J Chen (eds), Proceedings of the 35th Chinese Control Conference, CCC 2016., 7555084, Chinese Control Conference, CCC, vol. 2016-August, IEEE Computer Society, pp. 10926-10931, 35th Chinese Control Conference, CCC 2016, Chengdu, China, 27/07/16. https://doi.org/10.1109/ChiCC.2016.7555084

Hypersonic vehicle longitudinal control based on sliding mode observer and dynamic surface control. / Guo, Yuyan; Wang, Shixing; Xu, Bin et al.
Proceedings of the 35th Chinese Control Conference, CCC 2016. ed. / Jie Chen; Qianchuan Zhao; Jie Chen. IEEE Computer Society, 2016. p. 10926-10931 7555084 (Chinese Control Conference, CCC; Vol. 2016-August).

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

TY - GEN

T1 - Hypersonic vehicle longitudinal control based on sliding mode observer and dynamic surface control

AU - Guo, Yuyan

AU - Wang, Shixing

AU - Xu, Bin

AU - Hu, Xiaoxiang

AU - Yuan, Yuan

PY - 2016/8/26

Y1 - 2016/8/26

N2 - In this paper, a class of sliding mode observer and a dynamic surface control law are proposed for the longitudinal dynamics of hypersonic flight vehicle. The sliding mode observer is designed to estimate the angle of attack and flight path angle which are usually difficult to measure. Using the estimation results, the back-stepping-based dynamic surface control law is designed to avoid the explosion of complexity caused by continuous integration, and the control method is applied on the hypersonic vehicle longitudinal model to make the aircraft track the reference trajectory precisely. Simulation results have shown that the proposed methods perform well on the control and state estimation of hypersonic vehicle.

AB - In this paper, a class of sliding mode observer and a dynamic surface control law are proposed for the longitudinal dynamics of hypersonic flight vehicle. The sliding mode observer is designed to estimate the angle of attack and flight path angle which are usually difficult to measure. Using the estimation results, the back-stepping-based dynamic surface control law is designed to avoid the explosion of complexity caused by continuous integration, and the control method is applied on the hypersonic vehicle longitudinal model to make the aircraft track the reference trajectory precisely. Simulation results have shown that the proposed methods perform well on the control and state estimation of hypersonic vehicle.

KW - Back-stepping Control

KW - Dynamic Surface Control

KW - Hypersonic Flight Vehicle

KW - Sliding Mode Observer

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M3 - 会议稿件

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BT - Proceedings of the 35th Chinese Control Conference, CCC 2016

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A2 - Chen, Jie

PB - IEEE Computer Society

T2 - 35th Chinese Control Conference, CCC 2016

Y2 - 27 July 2016 through 29 July 2016

ER -

Hypersonic vehicle longitudinal control based on sliding mode observer and dynamic surface control

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