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Output-feedback based partial integrated missile guidance and control law design
1
作者
Xuejiao Sun
Rui Zhou
Delong Hou
《Journal of Systems Engineering and Electronics》
SCIE
EI
CSCD
2016年第6期1238-1248,共11页
An output-feedback based partial integrated guidance and control (IGC) law for missile interceptor is proposed with the smooth finite time convergence property. Firstly, a novel outputfeedback based smooth sliding mod...
An output-feedback based partial integrated guidance and control (IGC) law for missile interceptor is proposed with the smooth finite time convergence property. Firstly, a novel outputfeedback based smooth sliding mode control is proposed for a class of nonlinear systems in the presence of immeasurable state and disturbance. The finite time convergence property of this control scheme is proved based on the Lyapunov stability and homogeneous principle. Then, the proposed control method is applied to the design of partial IGC law. A kind of scaling methods is also developed to reach the rapid convergence of the system. An important dominance of this control scheme is the smooth characteristic, which may result in chattering free convergence. The simulation results indicate the high precision and smooth elevator deflection of the proposed output feedback base partial IGC law. © 2016 Beijing Institute of Aerospace Information.
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关键词
Control
system
synthesis
Control
theory
Electronic
guidance
systems
guided
missile
s
missile
s
Sliding
mode
control
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职称材料
题名
Output-feedback based partial integrated missile guidance and control law design
1
作者
Xuejiao Sun
Rui Zhou
Delong Hou
机构
School of Automation Science and Electrical Engineering
Beijing Institute of Electronic System Engineering
出处
《Journal of Systems Engineering and Electronics》
SCIE
EI
CSCD
2016年第6期1238-1248,共11页
基金
supported by the National Natural Science Foundation of China(61273349)
文摘
An output-feedback based partial integrated guidance and control (IGC) law for missile interceptor is proposed with the smooth finite time convergence property. Firstly, a novel outputfeedback based smooth sliding mode control is proposed for a class of nonlinear systems in the presence of immeasurable state and disturbance. The finite time convergence property of this control scheme is proved based on the Lyapunov stability and homogeneous principle. Then, the proposed control method is applied to the design of partial IGC law. A kind of scaling methods is also developed to reach the rapid convergence of the system. An important dominance of this control scheme is the smooth characteristic, which may result in chattering free convergence. The simulation results indicate the high precision and smooth elevator deflection of the proposed output feedback base partial IGC law. © 2016 Beijing Institute of Aerospace Information.
关键词
Control
system
synthesis
Control
theory
Electronic
guidance
systems
guided
missile
s
missile
s
Sliding
mode
control
Keywords
Control system synthesis
Control theory
Electronic guidance systems
guided missile
s
missile
s
Sliding mode control
分类号
TJ765 [兵器科学与技术—武器系统与运用工程]
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1
Output-feedback based partial integrated missile guidance and control law design
Xuejiao Sun
Rui Zhou
Delong Hou
《Journal of Systems Engineering and Electronics》
SCIE
EI
CSCD
2016
0
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