基于BP网络和DQN的预测-校正再入制导方法  

A prediction and correction reentry guidance method based on BP network and deep Q-learning network

作　　者：王宽 闫循良[1] 洪蓓 南汶江 王培臣 WANG Kuan;YAN Xunliang;HONG Bei;NAN Wenjiang;WANG Peichen(School of Astronautics,Northwestern Polytechnical University,Xi′an 710072,China;Beijing Institute of Astronautical Systems Engineering,Beijing 100076,China)

机构地区：[1]西北工业大学航天学院,陕西西安710072 [2]北京宇航系统工程研究所,北京100076

出　　处：《西北工业大学学报》2025年第2期201-211,共11页Journal of Northwestern Polytechnical University

基　　金：国家自然科学基金(11602296);陕西省自然科学基础研究计划(2019JM-434);智控实验室开放基金(2023-ZKSYS-KF04-02)资助。

摘　　要：针对传统数值预测-校正制导算法计算效率低、难以在线应用等问题,提出了一种基于BP网络和深度Q学习网络(DQN)的预测-校正制导方法。该方法采用纵、侧向制导解耦设计思想,在纵向制导方面,构建并训练了剩余航程预测BP网络,利用预测航程偏差校正倾侧角幅值剖面参数;在侧向制导方面,针对再入制导问题构建强化学习所需的状态、动作空间;确定决策点并设计考虑综合性能的奖励函数;构建强化学习训练网络,进而通过学习网络实现倾侧反转决策。以CAV-H再入滑翔为例进行仿真,结果表明:与传统数值预测-校正方法相比,所提基于BP网络的纵向制导方法具有相当的终端精度和较高的计算效率;与传统基于航向角走廊的侧向制导方法相比,所提基于DQN的侧向制导方法具有相当的计算精度以及更少的反转次数。A prediction and correction reentry guidance method based on the BP network and the deep Q-learning network(DQN)is proposed to address the issues of low computational efficiency and difficulty in the online application of a traditional numerical prediction and correction guidance algorithm.This method adopts the design concept of longitudinal and lateral guidance decoupling.For longitudinal guidance,a residual range prediction BP network is constructed and trained,and the predicted range deviation is used to correct the pitch angle profile parameters.For lateral guidance,firstly,the state and action space needed by the reinforcement learning are constructed to solve re-entry guidance problems.Secondly,the decision points are determined and the reward function that considers comprehensive performance is designed.The reinforcement learning training network is constructed to achieve tilt reversal decision-making through the learning network.Simulations are carried out with the CAV-H reentry gliding as example.The simulation results show that compared with the traditional numerical prediction and correction method,the longitudinal guidance method based on the BP network is significantly superior in terminal accuracy and computational efficiency.Compared with the traditional lateral guidance method based on the heading angle corridor,the lateral guidance method based on the DQN has considerable computational accuracy and fewer reversal times.

关 键 词：再入滑翔制导 预测-校正 BP网络 强化学习 深度Q学习网络 

分 类 号：V412.4[航空宇航科学与技术—航空宇航推进理论与工程]