Parametric approach for longitudinal attitude control of a hypersonic vehicle

Duan Guangren; Hu Yanmei; Tan Feng; Liu Wangkui

doi:10.1109/ChiCC.2015.7260541

Parametric approach for longitudinal attitude control of a hypersonic vehicle

Duan Guangren
, Hu Yanmei
, Tan Feng
, Liu Wangkui

School of Astronautics

Harbin Institute of Technology

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

Abstract

In this paper, a parametric approach for longitudinal attitude control of a hypersonic vehicle is presented. Firstly, according to the complicated aerodynamics characteristic of a hypersonic vehicle, the model of the pitch channel is treated as an interval system in order to cope with parameter uncertainties. Secondly, by employing robust stability analysis and parametric control theory, a parameterization of state feedback controllers for the interval autopilot system is obtained. Thirdly, by appropriately optimizing the free parameters in the robust stabilizing controller, the H₂ norm of the disturbance-output transfer function is made sufficiently small over the system parameter intervals. A simulation example of the pitch channel of a hypersonic vehicle demonstrates that the system achieves good performance with external disturbance despite the aerodynamical parameters vary in a large scale.

Original language	English
Title of host publication	Proceedings of the 34th Chinese Control Conference, CCC 2015
Editors	Qianchuan Zhao, Shirong Liu
Publisher	IEEE Computer Society
Pages	5776-5781
Number of pages	6
ISBN (Electronic)	9789881563897
DOIs	https://doi.org/10.1109/ChiCC.2015.7260541
State	Published - 11 Sep 2015
Event	34th Chinese Control Conference, CCC 2015 - Hangzhou, China Duration: 28 Jul 2015 → 30 Jul 2015

Publication series

Name	Chinese Control Conference, CCC
Volume	2015-September
ISSN (Print)	1934-1768
ISSN (Electronic)	2161-2927

Conference

Conference	34th Chinese Control Conference, CCC 2015
Country/Territory	China
City	Hangzhou
Period	28/07/15 → 30/07/15

Keywords

Disturbance Attenuation
Hypersonic Vehicle
Parametric Approach
Robust Stabilization

Access to Document

10.1109/ChiCC.2015.7260541

Cite this

Guangren, D., Yanmei, H., Feng, T., & Wangkui, L. (2015). Parametric approach for longitudinal attitude control of a hypersonic vehicle. In Q. Zhao, & S. Liu (Eds.), Proceedings of the 34th Chinese Control Conference, CCC 2015 (pp. 5776-5781). Article 7260541 (Chinese Control Conference, CCC; Vol. 2015-September). IEEE Computer Society. https://doi.org/10.1109/ChiCC.2015.7260541

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title = "Parametric approach for longitudinal attitude control of a hypersonic vehicle",

abstract = "In this paper, a parametric approach for longitudinal attitude control of a hypersonic vehicle is presented. Firstly, according to the complicated aerodynamics characteristic of a hypersonic vehicle, the model of the pitch channel is treated as an interval system in order to cope with parameter uncertainties. Secondly, by employing robust stability analysis and parametric control theory, a parameterization of state feedback controllers for the interval autopilot system is obtained. Thirdly, by appropriately optimizing the free parameters in the robust stabilizing controller, the H2 norm of the disturbance-output transfer function is made sufficiently small over the system parameter intervals. A simulation example of the pitch channel of a hypersonic vehicle demonstrates that the system achieves good performance with external disturbance despite the aerodynamical parameters vary in a large scale.",

keywords = "Disturbance Attenuation, Hypersonic Vehicle, Parametric Approach, Robust Stabilization",

author = "Duan Guangren and Hu Yanmei and Tan Feng and Liu Wangkui",

note = "Publisher Copyright: {\textcopyright} 2015 Technical Committee on Control Theory, Chinese Association of Automation.; 34th Chinese Control Conference, CCC 2015 ; Conference date: 28-07-2015 Through 30-07-2015",

year = "2015",

month = sep,

day = "11",

doi = "10.1109/ChiCC.2015.7260541",

language = "英语",

series = "Chinese Control Conference, CCC",

publisher = "IEEE Computer Society",

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address = "美国",

}

Guangren, D, Yanmei, H, Feng, T & Wangkui, L 2015, Parametric approach for longitudinal attitude control of a hypersonic vehicle. in Q Zhao & S Liu (eds), Proceedings of the 34th Chinese Control Conference, CCC 2015., 7260541, Chinese Control Conference, CCC, vol. 2015-September, IEEE Computer Society, pp. 5776-5781, 34th Chinese Control Conference, CCC 2015, Hangzhou, China, 28/07/15. https://doi.org/10.1109/ChiCC.2015.7260541

Parametric approach for longitudinal attitude control of a hypersonic vehicle. / Guangren, Duan; Yanmei, Hu; Feng, Tan et al.
Proceedings of the 34th Chinese Control Conference, CCC 2015. ed. / Qianchuan Zhao; Shirong Liu. IEEE Computer Society, 2015. p. 5776-5781 7260541 (Chinese Control Conference, CCC; Vol. 2015-September).

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

TY - GEN

T1 - Parametric approach for longitudinal attitude control of a hypersonic vehicle

AU - Guangren, Duan

AU - Yanmei, Hu

AU - Feng, Tan

AU - Wangkui, Liu

PY - 2015/9/11

Y1 - 2015/9/11

N2 - In this paper, a parametric approach for longitudinal attitude control of a hypersonic vehicle is presented. Firstly, according to the complicated aerodynamics characteristic of a hypersonic vehicle, the model of the pitch channel is treated as an interval system in order to cope with parameter uncertainties. Secondly, by employing robust stability analysis and parametric control theory, a parameterization of state feedback controllers for the interval autopilot system is obtained. Thirdly, by appropriately optimizing the free parameters in the robust stabilizing controller, the H2 norm of the disturbance-output transfer function is made sufficiently small over the system parameter intervals. A simulation example of the pitch channel of a hypersonic vehicle demonstrates that the system achieves good performance with external disturbance despite the aerodynamical parameters vary in a large scale.

AB - In this paper, a parametric approach for longitudinal attitude control of a hypersonic vehicle is presented. Firstly, according to the complicated aerodynamics characteristic of a hypersonic vehicle, the model of the pitch channel is treated as an interval system in order to cope with parameter uncertainties. Secondly, by employing robust stability analysis and parametric control theory, a parameterization of state feedback controllers for the interval autopilot system is obtained. Thirdly, by appropriately optimizing the free parameters in the robust stabilizing controller, the H2 norm of the disturbance-output transfer function is made sufficiently small over the system parameter intervals. A simulation example of the pitch channel of a hypersonic vehicle demonstrates that the system achieves good performance with external disturbance despite the aerodynamical parameters vary in a large scale.

KW - Disturbance Attenuation

KW - Hypersonic Vehicle

KW - Parametric Approach

KW - Robust Stabilization

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BT - Proceedings of the 34th Chinese Control Conference, CCC 2015

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PB - IEEE Computer Society

T2 - 34th Chinese Control Conference, CCC 2015

Y2 - 28 July 2015 through 30 July 2015

ER -

Parametric approach for longitudinal attitude control of a hypersonic vehicle

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