Journal of Projectiles, Rockets, Missiles and Guidance >
Terminal Adaptive Proportional Guidance Law for Guided Bomb
Received date: 2013-06-26
Online published: 2025-05-30
An adaptive proportional guidance law with angular constraint is developed for guided bomb, which meets the requirements of strap-down seeker and penetrating attack. Firstly, a gain variable proportional navigation guidance law was derived by classical proportional navigation and desired impact angle. Then, a closed-loop correction of guided coefficients was proposed for the sake of robustness enhance-ment of the guidance law. Simulation studies show that the presented guidance law can implement efficiently the angular constraint mission as well as preferable guidance precision.
LI Jiongliang , LIU Huaixun , WANG Hang , XUE Xiaodong . Terminal Adaptive Proportional Guidance Law for Guided Bomb[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014 , 34(6) : 54 -56,67 . DOI: 10.15892/j.cnki.djzdxb.2014.06.014
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