Aerodynamic and side jet compound control system design of intercept missiles using LPV techniques

Chang Zhu; Ke Mao Ma

Aerodynamic and side jet compound control system design of intercept missiles using LPV techniques

Chang Zhu^*
, Ke Mao Ma

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

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

Abstract

The compound control system of an intercept missile by means of combining the traditional aerodynamic control with reaction jets control is studied in this paper. Firstly, a LPV (linear parameter-varying) model is constructed, then, a linear parameter-varying aerodynamic controller is designed. At last, the design of the reaction jets control and switching instant of time is given, and simulation research is conducted. The simulation results show the effectiveness of the proposed approach.

Original language	English
Pages (from-to)	30-34
Number of pages	5
Journal	Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology
Volume	39
Issue number	SUPPL. 1
State	Published - Jun 2007

Keywords

Compound control
Intercept missile
LPV
Side-jet

Cite this

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title = "Aerodynamic and side jet compound control system design of intercept missiles using LPV techniques",

abstract = "The compound control system of an intercept missile by means of combining the traditional aerodynamic control with reaction jets control is studied in this paper. Firstly, a LPV (linear parameter-varying) model is constructed, then, a linear parameter-varying aerodynamic controller is designed. At last, the design of the reaction jets control and switching instant of time is given, and simulation research is conducted. The simulation results show the effectiveness of the proposed approach.",

keywords = "Compound control, Intercept missile, LPV, Side-jet",

author = "Chang Zhu and Ma, \{Ke Mao\}",

year = "2007",

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language = "英语",

volume = "39",

pages = "30--34",

journal = "Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology",

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T1 - Aerodynamic and side jet compound control system design of intercept missiles using LPV techniques

AU - Zhu, Chang

AU - Ma, Ke Mao

PY - 2007/6

Y1 - 2007/6

N2 - The compound control system of an intercept missile by means of combining the traditional aerodynamic control with reaction jets control is studied in this paper. Firstly, a LPV (linear parameter-varying) model is constructed, then, a linear parameter-varying aerodynamic controller is designed. At last, the design of the reaction jets control and switching instant of time is given, and simulation research is conducted. The simulation results show the effectiveness of the proposed approach.

AB - The compound control system of an intercept missile by means of combining the traditional aerodynamic control with reaction jets control is studied in this paper. Firstly, a LPV (linear parameter-varying) model is constructed, then, a linear parameter-varying aerodynamic controller is designed. At last, the design of the reaction jets control and switching instant of time is given, and simulation research is conducted. The simulation results show the effectiveness of the proposed approach.

KW - Compound control

KW - Intercept missile

KW - LPV

KW - Side-jet

UR - https://www.scopus.com/pages/publications/36549017206

M3 - 文章

AN - SCOPUS:36549017206

SN - 0367-6234

VL - 39

SP - 30

EP - 34

JO - Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology

JF - Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology

IS - SUPPL. 1

ER -

Aerodynamic and side jet compound control system design of intercept missiles using LPV techniques

Abstract

Keywords

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