Homing Guidance Law Design against Maneuvering Targets Based on DDPG

被引:2
|
作者
Liang, Yangang [1 ,2 ]
Tang, Jin [1 ,2 ]
Bai, Zhihui [3 ]
Li, Kebo [1 ,2 ]
机构
[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Peoples R China
[2] Hunan Key Lab Intelligent Planning & Simulat Aeros, Changsha 410073, Peoples R China
[3] 31102 Troops, Nanjing 210000, Peoples R China
基金
中国国家自然科学基金;
关键词
PROPORTIONAL NAVIGATION; PERFORMANCE; PPN; GO;
D O I
10.1155/2023/4188037
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A novel homing guidance law against maneuvering targets based on the deep deterministic policy gradient (DDPG) is proposed. The proposed guidance law directly maps the engagement state information to the acceleration of the interceptor, which is an end-to-end guidance policy. Firstly, the kinematic model of the interception process is described as a Markov decision process (MDP) that is applied to the deep reinforcement learning (DRL) algorithm. Then, an environment of training, state, action, and network structure is reasonably designed. Only the measurements of line-of-sight (LOS) angles and LOS rotational rates are used as state inputs, which can greatly simplify the problem of state estimation. Then, considering the LOS rotational rate and zero-effort-miss (ZEM), the Gaussian reward and terminal reward are designed to build a complete training and testing simulation environment. DDPG is used to deal with the RL problem to obtain a guidance law. Finally, the proposed RL guidance law's performance has been validated using numerical simulation examples. The proposed RL guidance law demonstrated improved performance compared to the classical true proportional navigation (TPN) method and the RL guidance policy using deep-Q-network (DQN).
引用
收藏
页数:12
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