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Homing Guidance Law of Anti-Ship Missiles Using Flight Path Angle  

Jin, Sheng-Hao (Dept. of Electronic Eng., Changwon National University)
Yang, Bin (Dept. of Electronic Eng., Changwon National University)
Hwang, Chung-Won (Dept. of Electronic Eng., Changwon National University)
Park, Seung-Yub (Dept. of Electronic Eng., Changwon National University)
Park, Seung-Je (LG Electronics HA Control R&D Lab.)
Publication Information
Journal of Advanced Navigation Technology / v.14, no.5, 2010 , pp. 596-603 More about this Journal
Abstract
This paper presents a homing guidance law of anti-ship missiles using flight path angle to achieve an impact time constraint as well as an impact angle constraint. the independent variable in the nonlinear engagement model is change d from the flight time to the heading angle of the missile. The proposed guidance law can home a missile to the target with zero miss distance as well as satisfying both of the impact angle and time constraints. The performance of the proposed guidance law is evaluated by the computer simulations.
Keywords
Impact Time Control; Angular Constraint; Flight Path Angle;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
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