Attitude control of missile via Fliess expansion and model predictive control

Yupeng Qiao; Baoqing Yang; Daizhan Cheng

doi:10.1109/WCICA.2008.4593146

Attitude control of missile via Fliess expansion and model predictive control

Yupeng Qiao^*
, Baoqing Yang
, Daizhan Cheng

^*Corresponding author for this work

School of Astronautics

CAS - Academy of Mathematics and System Sciences

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

7 Scopus citations

Abstract

This paper considers the attitude control of missile. We convert the problem into an output tracking one of nonlinear systems via control with finite admissible values. First, the Fliess functional expansion is used to describe the outputs. Then under piece-wise admissible value control and the quadratic criteria, the optimal control is obtained using model predictive control. The method developed is used to the attitude control of missile. Simulation results show the effectiveness of the proposed method.

Original language	English
Title of host publication	Proceedings of the 7th World Congress on Intelligent Control and Automation, WCICA'08
Pages	1527-1532
Number of pages	6
DOIs	https://doi.org/10.1109/WCICA.2008.4593146
State	Published - 2008
Event	7th World Congress on Intelligent Control and Automation, WCICA'08 - Chongqing, China Duration: 25 Jun 2008 → 27 Jun 2008

Publication series

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

Conference

Conference	7th World Congress on Intelligent Control and Automation, WCICA'08
Country/Territory	China
City	Chongqing
Period	25/06/08 → 27/06/08

Keywords

Attitude control of missile
Fliess functional expansion
Model predictive control

Access to Document

10.1109/WCICA.2008.4593146

Cite this

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title = "Attitude control of missile via Fliess expansion and model predictive control",

abstract = "This paper considers the attitude control of missile. We convert the problem into an output tracking one of nonlinear systems via control with finite admissible values. First, the Fliess functional expansion is used to describe the outputs. Then under piece-wise admissible value control and the quadratic criteria, the optimal control is obtained using model predictive control. The method developed is used to the attitude control of missile. Simulation results show the effectiveness of the proposed method.",

keywords = "Attitude control of missile, Fliess functional expansion, Model predictive control",

author = "Yupeng Qiao and Baoqing Yang and Daizhan Cheng",

year = "2008",

doi = "10.1109/WCICA.2008.4593146",

language = "英语",

isbn = "9781424421145",

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

pages = "1527--1532",

booktitle = "Proceedings of the 7th World Congress on Intelligent Control and Automation, WCICA'08",

note = "7th World Congress on Intelligent Control and Automation, WCICA'08 ; Conference date: 25-06-2008 Through 27-06-2008",

}

Qiao, Y, Yang, B & Cheng, D 2008, Attitude control of missile via Fliess expansion and model predictive control. in Proceedings of the 7th World Congress on Intelligent Control and Automation, WCICA'08., 4593146, Proceedings of the World Congress on Intelligent Control and Automation (WCICA), pp. 1527-1532, 7th World Congress on Intelligent Control and Automation, WCICA'08, Chongqing, China, 25/06/08. https://doi.org/10.1109/WCICA.2008.4593146

Attitude control of missile via Fliess expansion and model predictive control. / Qiao, Yupeng; Yang, Baoqing; Cheng, Daizhan.
Proceedings of the 7th World Congress on Intelligent Control and Automation, WCICA'08. 2008. p. 1527-1532 4593146 (Proceedings of the World Congress on Intelligent Control and Automation (WCICA)).

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

TY - GEN

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AU - Qiao, Yupeng

AU - Yang, Baoqing

AU - Cheng, Daizhan

PY - 2008

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N2 - This paper considers the attitude control of missile. We convert the problem into an output tracking one of nonlinear systems via control with finite admissible values. First, the Fliess functional expansion is used to describe the outputs. Then under piece-wise admissible value control and the quadratic criteria, the optimal control is obtained using model predictive control. The method developed is used to the attitude control of missile. Simulation results show the effectiveness of the proposed method.

AB - This paper considers the attitude control of missile. We convert the problem into an output tracking one of nonlinear systems via control with finite admissible values. First, the Fliess functional expansion is used to describe the outputs. Then under piece-wise admissible value control and the quadratic criteria, the optimal control is obtained using model predictive control. The method developed is used to the attitude control of missile. Simulation results show the effectiveness of the proposed method.

KW - Attitude control of missile

KW - Fliess functional expansion

KW - Model predictive control

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DO - 10.1109/WCICA.2008.4593146

M3 - 会议稿件

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T3 - Proceedings of the World Congress on Intelligent Control and Automation (WCICA)

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BT - Proceedings of the 7th World Congress on Intelligent Control and Automation, WCICA'08

T2 - 7th World Congress on Intelligent Control and Automation, WCICA'08

Y2 - 25 June 2008 through 27 June 2008

ER -

Attitude control of missile via Fliess expansion and model predictive control

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Keywords

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