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Journal of Projectiles, Rockets, Missiles and Guidance >
Optimal Evasion Trajectory of an Uncertain Guided Air Combat Missile
Received date: 2009-05-13
Online published: 2025-05-28
The evasion of guided missiles is crucial for the survival in air combat. A new model was introduced for the optimal solu-tion of the missile avoidance problem under uncertainty. The model consists of the identification and control phases. In the first phase, the target's belief in the guidance law of the missile was updated using Bayesian reasoning. In the second phase, the con-trols of the aircraft were solved using the receding horizon control scheme. The simulation results show the model is effective.
Key words： maneuvering evasion; guidance law; uncertainty
HU Anhui , ZHENG Tao , ZHU Shigang , GAO Wei . Optimal Evasion Trajectory of an Uncertain Guided Air Combat Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(3) : 32 -34 . DOI: 10.15892/j.cnki.djzdxb.2010.03.075
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