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针对强机动目标三维拦截的混合残差强化学习方法

徐天行1,方东洋2,3,南英1,张谋富1   

  1. 1. 南京航空航天大学
    2. 南京航空航天大学航天学院
    3. 上海机电工程研究所
  • 收稿日期:2026-05-21 修回日期:2026-09-04 出版日期:2026-09-10 发布日期:2026-09-10
  • 通讯作者: 南英

Hybrid Residual Reinforcement Learning for 3D Interception of Highly Maneuvering Targets

  • Received:2026-05-21 Revised:2026-09-04 Online:2026-09-10 Published:2026-09-10
  • Contact: Ying NAN

摘要: 针对强机动目标三维末制导中经典比例导引存在制导迟滞、带补偿比例导引依赖目标真实精确加速度、纯强化学习制导训练难度大且易出现尾部失效等问题,提出一种融合比例导引物理先验与近端策略优化算法的混合残差强化学习制导方法。该方法以比例导引作为名义制导基线,由强化学习智能体输出有限幅乘性残差增益,对比例导引指令进行动态修正;当网络输出为零时,制导律可退化为传统比例导引,从而保留PNG指令结构以及网络零输出条件下向PNG退化的能力,并降低端到端强化学习的探索难度。为增强智能体对强机动目标运动趋势和视线角速率变化规律的感知能力,构造时序帧堆叠状态表征,并在训练过程中采用动态熵衰减策略调节探索强度;同时在仿真环境中考虑自动驾驶仪一阶惯性和过载限幅约束,以提高制导模型与工程约束的一致性。仿真结果表明,在蛇形机动和动态多级随机机动场景下,所提方法相比传统比例导引和带补偿比例导引能够有效降低脱靶量;相较纯强化学习方法,虽然在固定机动模式下极限精度不占优势,但在动态随机强机动场景中能够降低长尾脱靶风险,表现出更好的最差工况稳定性。消融实验表明,时序帧堆叠是提升制导性能和鲁棒性的主要因素,动态熵衰减对训练过程具有一定调节作用,而末端平滑衰减在本文任务设定下会削弱末端残差修正能力,因此最终方法采用无末端平滑衰减的混合残差制导结构。

关键词: 深度强化学习, 残差控制, 末制导, 比例导引, 强机动目标

Abstract: To address the three-dimensional terminal guidance problem against highly maneuvering targets, this paper proposes a hybrid residual reinforcement learning guidance method that combines physics-based prior embedded in proportional navigation guidance (PNG) with proximal policy optimization. The proposed method takes proportional navigation guidance as the nominal baseline, while the reinforcement learning agent outputs bounded multiplicative residual gains to dynamically modify the baseline guidance command. When the neural network output is zero, the guidance law reduces to conventional PNG, thereby preserving the PNG command structure and enabling reversion to PNG under zero network output, while reducing the exploration burden of end-to-end reinforcement learning. To improve the agent’s perception of target maneuvering trends and line-of-sight rate variations, a temporal frame-stacking state representation is constructed. A dynamic entropy-coefficient decay strategy is adopted during training to regulate exploration, and first-order autopilot lag and overload saturation constraints are included in the simulation environment to improve consistency with engineering conditions. Simulation results show that, under both weaving and dynamic multi-stage random maneuver scenarios, the proposed method effectively reduces the miss distance compared with conventional proportional navigation guidance and augmented proportional navigation guidance. Although the proposed method does not achieve the lowest miss distance obtained by pure reinforcement learning guidance in the fixed maneuver case, it suppresses long-tail miss-distance risk in dynamic random maneuver scenarios and exhibits better worst-case stability. Ablation results indicate that temporal frame stacking is the main contributor to the improvement of guidance performance and robustness, while dynamic entropy-coefficient decay mainly regulates the exploration process during training. In contrast, terminal residual attenuation did not provide consistent performance gains and slightly weakened the terminal residual correction capability under the task setting of this paper; therefore, the final method adopts a hybrid residual guidance structure without terminal residual attenuation.

Key words: Deep Reinforcement Learning, Residual Control, Terminal Guidance, Proportional Navigation, Highly Maneuvering Targets

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