Journal of Projectiles, Rockets, Missiles and Guidance >
The Research on Optimal Proportional Navigation Guidance with Single Dynamic Lag
Received date: 2010-10-27
Online published: 2025-05-30
The guidance model with single dynamic lag was established. The optimal guidance law with single time constant was deduced using optimal theory. The research on proportional navigation, augmented proportional navigation and optimal guidance law was done. It is concluded that the optimal guidance law with single time constant can reduce the demand of acceleration at the terminal of the trajectory and reduce the demand of guidance time, and this optimal guidance law can reduce the influence of dynamic lag on miss distance.
WANG Hui , LIN Defu , CHENG Zhenxuan . The Research on Optimal Proportional Navigation Guidance with Single Dynamic Lag[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(4) : 33 -36 . DOI: 10.15892/j.cnki.djzdxb.2011.04.013
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