H∞ gain-scheduled missile controller design using linear parameter-varying feedback

Yu Jianqiao; Liu Li; Zhao Hongxia; Xu Chengdong

doi:10.1109/ICICIC.2006.93

H_∞ gain-scheduled missile controller design using linear parameter-varying feedback

Yu Jianqiao^*, Liu Li, Zhao Hongxia, Xu Chengdong

^*Corresponding author for this work

School of Aerospace Engineering

Beijing Institute of Technology

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

Abstract

The dynamic characteristics of missile vary substantially with flight conditions such as flight Mach number, altitude and angle of attack. Therefore, in order to achieve adequate levels of robustness and performance, a controller that also varies during operation has to be designed in missile control. This paper is concerned with the application of advanced mixed linear parameter-varying (LPV)/μ techniques to global control of a missile. The techniques can produce an H_∞ based LPV controller, which is automatically "gain scheduled" with respect to the flight conditions and adapts to the variation of the missile's dynamic characteristics. The power and effectiveness of the resulting controller are demonstrated by nonlinear simulations.

Original language	English
Title of host publication	First International Conference on Innovative Computing, Information and Control 2006, ICICIC'06
Pages	686-689
Number of pages	4
DOIs	https://doi.org/10.1109/ICICIC.2006.93
Publication status	Published - 2006
Event	1st International Conference on Innovative Computing, Information and Control 2006, ICICIC'06 - Beijing, United States Duration: 30 Aug 2006 → 1 Sept 2006

Publication series

Name	First International Conference on Innovative Computing, Information and Control 2006, ICICIC'06

Conference

Conference	1st International Conference on Innovative Computing, Information and Control 2006, ICICIC'06
Country/Territory	United States
City	Beijing
Period	30/08/06 → 1/09/06

Access to Document

10.1109/ICICIC.2006.93

Cite this

Jianqiao, Y., Li, L., Hongxia, Z., & Chengdong, X. (2006). H_∞ gain-scheduled missile controller design using linear parameter-varying feedback. In First International Conference on Innovative Computing, Information and Control 2006, ICICIC'06 (pp. 686-689). Article 1691892 (First International Conference on Innovative Computing, Information and Control 2006, ICICIC'06). https://doi.org/10.1109/ICICIC.2006.93

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title = "H∞ gain-scheduled missile controller design using linear parameter-varying feedback",

abstract = "The dynamic characteristics of missile vary substantially with flight conditions such as flight Mach number, altitude and angle of attack. Therefore, in order to achieve adequate levels of robustness and performance, a controller that also varies during operation has to be designed in missile control. This paper is concerned with the application of advanced mixed linear parameter-varying (LPV)/μ techniques to global control of a missile. The techniques can produce an H∞ based LPV controller, which is automatically {"}gain scheduled{"} with respect to the flight conditions and adapts to the variation of the missile's dynamic characteristics. The power and effectiveness of the resulting controller are demonstrated by nonlinear simulations.",

author = "Yu Jianqiao and Liu Li and Zhao Hongxia and Xu Chengdong",

year = "2006",

doi = "10.1109/ICICIC.2006.93",

language = "English",

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series = "First International Conference on Innovative Computing, Information and Control 2006, ICICIC'06",

pages = "686--689",

booktitle = "First International Conference on Innovative Computing, Information and Control 2006, ICICIC'06",

note = "1st International Conference on Innovative Computing, Information and Control 2006, ICICIC'06 ; Conference date: 30-08-2006 Through 01-09-2006",

}

Jianqiao, Y , Li, L, Hongxia, Z & Chengdong, X 2006, H_∞ gain-scheduled missile controller design using linear parameter-varying feedback. in First International Conference on Innovative Computing, Information and Control 2006, ICICIC'06., 1691892, First International Conference on Innovative Computing, Information and Control 2006, ICICIC'06, pp. 686-689, 1st International Conference on Innovative Computing, Information and Control 2006, ICICIC'06, Beijing, United States, 30/08/06. https://doi.org/10.1109/ICICIC.2006.93

H_∞ gain-scheduled missile controller design using linear parameter-varying feedback. / Jianqiao, Yu ; Li, Liu; Hongxia, Zhao et al.
First International Conference on Innovative Computing, Information and Control 2006, ICICIC'06. 2006. p. 686-689 1691892 (First International Conference on Innovative Computing, Information and Control 2006, ICICIC'06).

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

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N2 - The dynamic characteristics of missile vary substantially with flight conditions such as flight Mach number, altitude and angle of attack. Therefore, in order to achieve adequate levels of robustness and performance, a controller that also varies during operation has to be designed in missile control. This paper is concerned with the application of advanced mixed linear parameter-varying (LPV)/μ techniques to global control of a missile. The techniques can produce an H∞ based LPV controller, which is automatically "gain scheduled" with respect to the flight conditions and adapts to the variation of the missile's dynamic characteristics. The power and effectiveness of the resulting controller are demonstrated by nonlinear simulations.

AB - The dynamic characteristics of missile vary substantially with flight conditions such as flight Mach number, altitude and angle of attack. Therefore, in order to achieve adequate levels of robustness and performance, a controller that also varies during operation has to be designed in missile control. This paper is concerned with the application of advanced mixed linear parameter-varying (LPV)/μ techniques to global control of a missile. The techniques can produce an H∞ based LPV controller, which is automatically "gain scheduled" with respect to the flight conditions and adapts to the variation of the missile's dynamic characteristics. The power and effectiveness of the resulting controller are demonstrated by nonlinear simulations.

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Jianqiao Y , Li L, Hongxia Z, Chengdong X. H_∞ gain-scheduled missile controller design using linear parameter-varying feedback. In First International Conference on Innovative Computing, Information and Control 2006, ICICIC'06. 2006. p. 686-689. 1691892. (First International Conference on Innovative Computing, Information and Control 2006, ICICIC'06). doi: 10.1109/ICICIC.2006.93