

系统工程与电子技术 ›› 2026, Vol. 48 ›› Issue (2): 694-704.doi: 10.12305/j.issn.1001-506X.2026.02.29
王旭, 蔡光斌, 余晓亚, 叶子绮, 单斌
收稿日期:2025-01-15
修回日期:2025-03-06
出版日期:2025-06-10
发布日期:2025-06-10
通讯作者:
蔡光斌
作者简介:王 旭(1998—),男,硕士研究生,主要研究方向为飞行器智能控制、人工智能基金资助:Xu WANG, Guangbin CAI, Xiaoya YU, Ziqi YE, Bin SHAN
Received:2025-01-15
Revised:2025-03-06
Online:2025-06-10
Published:2025-06-10
Contact:
Guangbin CAI
摘要:
针对高超声速飞行器姿态控制中的强非线性和大不确定性特点,以及传统强化学习算法在多重控制需求下训练收敛性和控制精度的不足,提出一种双动态自适应近端策略优化(proximal policy optimization, PPO)算法。算法通过软动态裁剪机制和策略驱动的熵调整机制,实现控制精度与执行机构保护的平衡,并在此基础上构建了集成气动特性和执行机构特性的综合仿真验证环境。结合比例-积分-微分控制思想,对状态观测空间进行了优化设计。仿真结果表明,与基准PPO算法相比,所提算法的收敛速度提升了22%,并显著改善了控制精度和动作平滑性。在不同飞行工况下,该方法展现出优异的策略适应性和鲁棒性,有效提升了飞行器的姿态控制性能。
中图分类号:
王旭, 蔡光斌, 余晓亚, 叶子绮, 单斌. 基于双动态PPO算法的高超声速飞行器姿态控制[J]. 系统工程与电子技术, 2026, 48(2): 694-704.
Xu WANG, Guangbin CAI, Xiaoya YU, Ziqi YE, Bin SHAN. Attitude control of hypersonic vehicle based on dual-dynamic PPO algorithm[J]. Systems Engineering and Electronics, 2026, 48(2): 694-704.
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