Homing Guidance Law Design against Maneuvering Targets Based on DDPG

IF 1.1 4区 工程技术 Q3 ENGINEERING, AEROSPACE International Journal of Aerospace Engineering Pub Date : 2023-06-13 DOI:10.1155/2023/4188037
Yan Liang, Jin Tang, Zhihui Bai, Kebo Li
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Abstract

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).
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基于DDPG的机动目标寻的制导律设计
提出了一种新的基于深度确定性策略梯度(DDPG)的机动目标寻的制导律。所提出的制导律直接将交战状态信息映射到拦截器的加速度,这是一种端到端的制导策略。首先,将拦截过程的运动学模型描述为应用于深度强化学习(DRL)算法的马尔可夫决策过程(MDP)。然后,合理地设计了训练、状态、动作和网络结构的环境。只有视线角和视线旋转率的测量值被用作状态输入,这可以极大地简化状态估计问题。然后,考虑到服务水平旋转率和零失误(ZEM),设计了高斯奖励和终端奖励,以建立一个完整的训练和测试模拟环境。DDPG用于处理RL问题以获得指导律。最后,通过数值仿真实例验证了所提出的RL制导律的性能。与经典的真比例导航(TPN)方法和使用深度Q网络(DQN)的RL制导策略相比,所提出的RL制导律表现出了改进的性能。
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来源期刊
CiteScore
2.70
自引率
7.10%
发文量
195
审稿时长
22 weeks
期刊介绍: International Journal of Aerospace Engineering aims to serve the international aerospace engineering community through dissemination of scientific knowledge on practical engineering and design methodologies pertaining to aircraft and space vehicles. Original unpublished manuscripts are solicited on all areas of aerospace engineering including but not limited to: -Mechanics of materials and structures- Aerodynamics and fluid mechanics- Dynamics and control- Aeroacoustics- Aeroelasticity- Propulsion and combustion- Avionics and systems- Flight simulation and mechanics- Unmanned air vehicles (UAVs). Review articles on any of the above topics are also welcome.
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