Robust controller design for autopilot of ABTT missile

Feng Tan; Guangren Duan; Lijun Zhao

doi:10.1109/WCICA.2006.1714308

Robust controller design for autopilot of ABTT missile

Feng Tan^*
, Guangren Duan
, Lijun Zhao

^*Corresponding author for this work

School of Astronautics

Harbin Engineering University

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

15 Scopus citations

Abstract

In this paper, a constant non-switching feedback controller, which stabilizes the system on the whole trajectory and doesn't vary with the rolling rate, is proposed according to the parameterized eigenstructure assignment method for the pitch/yaw channel autopilot of a certain BTT missile. Feedforward compensators are designed based on the model reference method to realize the tracking of the overload signals. The stability of the designed autopilot is strictly analyzed based on the theory of quadratic stability and the resulted system is proved to be robust stable against variations of the rolling rate and system parameters. The structure of the proposed controller is very simple and can be easily realized. Simulation results show the effect of the method.

Original language	English
Title of host publication	Proceedings of the World Congress on Intelligent Control and Automation (WCICA)
Pages	6358-6362
Number of pages	5
DOIs	https://doi.org/10.1109/WCICA.2006.1714308
State	Published - 2006
Event	6th World Congress on Intelligent Control and Automation, WCICA 2006 - Dalian, China Duration: 21 Jun 2006 → 23 Jun 2006

Publication series

Name	Proceedings of the World Congress on Intelligent Control and Automation (WCICA)
Volume	2

Conference

Conference	6th World Congress on Intelligent Control and Automation, WCICA 2006
Country/Territory	China
City	Dalian
Period	21/06/06 → 23/06/06

Keywords

Autopilot
BTT
Eigenstructure assignment
Robust stabilization
System family

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10.1109/WCICA.2006.1714308

Cite this

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title = "Robust controller design for autopilot of ABTT missile",

abstract = "In this paper, a constant non-switching feedback controller, which stabilizes the system on the whole trajectory and doesn't vary with the rolling rate, is proposed according to the parameterized eigenstructure assignment method for the pitch/yaw channel autopilot of a certain BTT missile. Feedforward compensators are designed based on the model reference method to realize the tracking of the overload signals. The stability of the designed autopilot is strictly analyzed based on the theory of quadratic stability and the resulted system is proved to be robust stable against variations of the rolling rate and system parameters. The structure of the proposed controller is very simple and can be easily realized. Simulation results show the effect of the method.",

keywords = "Autopilot, BTT, Eigenstructure assignment, Robust stabilization, System family",

author = "Feng Tan and Guangren Duan and Lijun Zhao",

year = "2006",

doi = "10.1109/WCICA.2006.1714308",

language = "英语",

isbn = "1424403324",

series = "Proceedings of the World Congress on Intelligent Control and Automation (WCICA)",

pages = "6358--6362",

booktitle = "Proceedings of the World Congress on Intelligent Control and Automation (WCICA)",

note = "6th World Congress on Intelligent Control and Automation, WCICA 2006 ; Conference date: 21-06-2006 Through 23-06-2006",

}

Tan, F , Duan, G & Zhao, L 2006, Robust controller design for autopilot of ABTT missile. in Proceedings of the World Congress on Intelligent Control and Automation (WCICA)., 1714308, Proceedings of the World Congress on Intelligent Control and Automation (WCICA), vol. 2, pp. 6358-6362, 6th World Congress on Intelligent Control and Automation, WCICA 2006, Dalian, China, 21/06/06. https://doi.org/10.1109/WCICA.2006.1714308

Robust controller design for autopilot of ABTT missile. / Tan, Feng ; Duan, Guangren; Zhao, Lijun.
Proceedings of the World Congress on Intelligent Control and Automation (WCICA). 2006. p. 6358-6362 1714308 (Proceedings of the World Congress on Intelligent Control and Automation (WCICA); Vol. 2).

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

TY - GEN

T1 - Robust controller design for autopilot of ABTT missile

AU - Tan, Feng

AU - Duan, Guangren

AU - Zhao, Lijun

PY - 2006

Y1 - 2006

N2 - In this paper, a constant non-switching feedback controller, which stabilizes the system on the whole trajectory and doesn't vary with the rolling rate, is proposed according to the parameterized eigenstructure assignment method for the pitch/yaw channel autopilot of a certain BTT missile. Feedforward compensators are designed based on the model reference method to realize the tracking of the overload signals. The stability of the designed autopilot is strictly analyzed based on the theory of quadratic stability and the resulted system is proved to be robust stable against variations of the rolling rate and system parameters. The structure of the proposed controller is very simple and can be easily realized. Simulation results show the effect of the method.

AB - In this paper, a constant non-switching feedback controller, which stabilizes the system on the whole trajectory and doesn't vary with the rolling rate, is proposed according to the parameterized eigenstructure assignment method for the pitch/yaw channel autopilot of a certain BTT missile. Feedforward compensators are designed based on the model reference method to realize the tracking of the overload signals. The stability of the designed autopilot is strictly analyzed based on the theory of quadratic stability and the resulted system is proved to be robust stable against variations of the rolling rate and system parameters. The structure of the proposed controller is very simple and can be easily realized. Simulation results show the effect of the method.

KW - Autopilot

KW - BTT

KW - Eigenstructure assignment

KW - Robust stabilization

KW - System family

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M3 - 会议稿件

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BT - Proceedings of the World Congress on Intelligent Control and Automation (WCICA)

T2 - 6th World Congress on Intelligent Control and Automation, WCICA 2006

Y2 - 21 June 2006 through 23 June 2006

ER -

Robust controller design for autopilot of ABTT missile

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Conference

Keywords

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