Robust stability analysis for a cruise missile This project was supported by the National Natural Science Foundation of China (60674101) and the Education University Doctor Foundation of Chinese Ministry (20050213010).

Shi Yingjing; Ma Guangfu; Ma Hongzhong

doi:10.1016/S1004-4132(08)60154-1

Robust stability analysis for a cruise missile This project was supported by the National Natural Science Foundation of China (60674101) and the Education University Doctor Foundation of Chinese Ministry (20050213010).

Shi Yingjing^*
, Ma Guangfu
, Ma Hongzhong

^*Corresponding author for this work

School of Astronautics, Harbin Institute of Technology
Industry Corporation

Research output: Contribution to journal › Article › peer-review

4 Scopus citations

Abstract

A global controller design methodology for a flight stage of the cruise missile is proposed. This methodology is based on the method of least squares. To prove robust stability in the full airspace with parameter disturbances, the concepts of convex polytopic models and quadratic stability are introduced. The effect of aerodynamic parameters on system performance is analyzed. The designed controller is applied to track the over-loading signal of the cruise segment of the cruise missile, avoiding system disturbance owing to controller switching. Simulation results demonstrate the validity of the proposed method.

Original language	English
Pages (from-to)	785-790
Number of pages	6
Journal	Journal of Systems Engineering and Electronics
Volume	19
Issue number	4
DOIs	https://doi.org/10.1016/S1004-4132(08)60154-1
State	Published - Aug 2008
Externally published	Yes

Keywords

aircraft control
least square
quadratic stabilization
robust control

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Yingjing, S., Guangfu, M., & Hongzhong, M. (2008). Robust stability analysis for a cruise missile This project was supported by the National Natural Science Foundation of China (60674101) and the Education University Doctor Foundation of Chinese Ministry (20050213010). Journal of Systems Engineering and Electronics, 19(4), 785-790. https://doi.org/10.1016/S1004-4132(08)60154-1

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title = "Robust stability analysis for a cruise missile This project was supported by the National Natural Science Foundation of China (60674101) and the Education University Doctor Foundation of Chinese Ministry (20050213010).",

abstract = "A global controller design methodology for a flight stage of the cruise missile is proposed. This methodology is based on the method of least squares. To prove robust stability in the full airspace with parameter disturbances, the concepts of convex polytopic models and quadratic stability are introduced. The effect of aerodynamic parameters on system performance is analyzed. The designed controller is applied to track the over-loading signal of the cruise segment of the cruise missile, avoiding system disturbance owing to controller switching. Simulation results demonstrate the validity of the proposed method.",

keywords = "aircraft control, least square, quadratic stabilization, robust control",

author = "Shi Yingjing and Ma Guangfu and Ma Hongzhong",

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Yingjing, S, Guangfu, M & Hongzhong, M 2008, 'Robust stability analysis for a cruise missile This project was supported by the National Natural Science Foundation of China (60674101) and the Education University Doctor Foundation of Chinese Ministry (20050213010).', Journal of Systems Engineering and Electronics, vol. 19, no. 4, pp. 785-790. https://doi.org/10.1016/S1004-4132(08)60154-1

Robust stability analysis for a cruise missile This project was supported by the National Natural Science Foundation of China (60674101) and the Education University Doctor Foundation of Chinese Ministry (20050213010). / Yingjing, Shi; Guangfu, Ma; Hongzhong, Ma.
In: Journal of Systems Engineering and Electronics, Vol. 19, No. 4, 08.2008, p. 785-790.

Research output: Contribution to journal › Article › peer-review

TY - JOUR

T1 - Robust stability analysis for a cruise missile This project was supported by the National Natural Science Foundation of China (60674101) and the Education University Doctor Foundation of Chinese Ministry (20050213010).

AU - Yingjing, Shi

AU - Guangfu, Ma

AU - Hongzhong, Ma

PY - 2008/8

Y1 - 2008/8

N2 - A global controller design methodology for a flight stage of the cruise missile is proposed. This methodology is based on the method of least squares. To prove robust stability in the full airspace with parameter disturbances, the concepts of convex polytopic models and quadratic stability are introduced. The effect of aerodynamic parameters on system performance is analyzed. The designed controller is applied to track the over-loading signal of the cruise segment of the cruise missile, avoiding system disturbance owing to controller switching. Simulation results demonstrate the validity of the proposed method.

AB - A global controller design methodology for a flight stage of the cruise missile is proposed. This methodology is based on the method of least squares. To prove robust stability in the full airspace with parameter disturbances, the concepts of convex polytopic models and quadratic stability are introduced. The effect of aerodynamic parameters on system performance is analyzed. The designed controller is applied to track the over-loading signal of the cruise segment of the cruise missile, avoiding system disturbance owing to controller switching. Simulation results demonstrate the validity of the proposed method.

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KW - least square

KW - quadratic stabilization

KW - robust control

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JF - Journal of Systems Engineering and Electronics

IS - 4

ER -

Robust stability analysis for a cruise missile This project was supported by the National Natural Science Foundation of China (60674101) and the Education University Doctor Foundation of Chinese Ministry (20050213010).

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Keywords

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