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Supervised by Ministry of Industry and Information Technology of The People's Republic of China Sponsored by Harbin Institute of Technology Editor-in-chief Yu Zhou ISSNISSN 1005-9113 CNCN 23-1378/T

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Related citation:GE Lian-zheng,ShenYi,XU Guang-chi.HP nonlinear guidance law design based on smooth sliding mode control[J].Journal of Harbin Institute Of Technology(New Series),2009,16(3):382-385.DOI:10.11916/j.issn.1005-9113.2009.03.016.
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HP nonlinear guidance law design based on smooth sliding mode control
Author NameAffiliation
GE Lian-zheng Dept. of Control Science and Engineering,Harbin Institute of Technology,Harbin 150001,China 
ShenYi Dept. of Control Science and Engineering,Harbin Institute of Technology,Harbin 150001,China 
XU Guang-chi Dept. of Control Science and Engineering,Harbin Institute of Technology,Harbin 150001,China 
Abstract:
To eliminate the perturbation of interceptor detection induced by aerodynamic heating,the head pursuit (HP) guidance law for three-dimensional interception was presented. The guidance law positioned the interceptor ahead of the target on its flight trajectory,and the speed of interceptor was required to be lower than that of the target. On the basis of a novel head pursuit three-dimensional guidance model,a nonlinear guidance law was developed based on smooth sliding mode control theory. At the same time,a special observer was designed to estimate the target acceleration,and a numerical example on maneuvering ballistic target interception verified the effectiveness of the presented guidance law.
Key words:  aerodynamic heating  three-dimensional interception  second-order sliding mode  observer
DOI：10.11916/j.issn.1005-9113.2009.03.016
Clc Number:TJ765.2
Fund:

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