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http://dx.doi.org/10.12673/jkoni.2012.16.1.008

Guidance Law of Missiles for Control Impact-Time-and-Angle by Flight Path Angle in Three Dimensional Space  

Jin, Sheng-Hao (Dept. of Electronic Eng., Changwon National University)
Lee, Chun-Gi (Dept. of Electronic Eng., Changwon National University)
Yang, Bin (Dept. of Electronic Eng., Changwon National University)
Hwan, Chung-Won (Dept. of Electrical Eng., Masan University)
Park, Seung-Yub (Dept. of Electronic Eng., Changwon National University)
Publication Information
Journal of Advanced Navigation Technology / v.16, no.1, 2012 , pp. 8-15 More about this Journal
Abstract
This paper on the assumption that the target is stationary and the velocity of missile is fixed value. In three dimensional space. Using flight path angle to simultaneous control impact-time-and-angle base on a homing guidance law. The independent variable in the nonlinear engagement model is the flight path angle of the missile. The propose homing guidance law can see the controllability of impact-time-and-angle. And also can see the processing of the missile arrive at the target. It is applied to several salvo attack scenarios. The performance of the proposed guidance law is verified by simulations.
Keywords
Three Dimensional; Angular Constraint; Flight Path Angle; Impact Time Control;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
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