Acta Aeronautica et Astronautica Sinica ›› 2026, Vol. 47 ›› Issue (8): 332753.doi: 10.7527/S1000-6893.2025.32753
• Electronics and Electrical Engineering and Control • Previous Articles
Hao ZHANG, Jianing LIU, Zhi XU(
), Yuanxin YANG
Received:2025-09-03
Revised:2025-09-18
Accepted:2025-11-08
Online:2025-12-16
Published:2025-11-20
Contact:
Zhi XU
E-mail:xuzhi@nwpu.edu.cn
CLC Number:
Hao ZHANG, Jianing LIU, Zhi XU, Yuanxin YANG. Trajectory prediction method of incoming missiles based on improved inverse reinforcement learning in aircraft active defense mode[J]. Acta Aeronautica et Astronautica Sinica, 2026, 47(8): 332753.
Table 4
Different prediction mode performance
| 载机机动形式 | 预测算法 | 10 s内/m | 40 s内/m |
|---|---|---|---|
| 匀速直线 | IMM滤波辨识算法 | 274.213 1 | 550.465 |
| AIRL方法 | 218.457 | 439.824 | |
| LSTM-Transformer模型 | 211.052 | 424.968 | |
| 所提算法 | 162.065 | 394.599 | |
| S型机动 | IMM滤波辨识算法 | 258.143 | 677.651 |
| AIRL方法 | 202.556 | 561.726 | |
| LSTM-Transformer模型 | 183.210 | 507.288 | |
| 所提算法 | 157.624 | 494.523 | |
| 掉头置尾 | IMM滤波辨识算法 | 234.227 | 501.584 |
| AIRL方法 | 213.385 | 452.283 | |
| LSTM-Transformer模型 | 208.617 | 431.499 | |
| 所提算法 | 170.706 | 393.720 |
Table C1
Neural network architecture and parameter design of baseline method
| 模型类型 | 网络模块 | 输入内容 | 输出内容 | 隐藏层配置 | 特殊结构 / 机制 |
|---|---|---|---|---|---|
| AIRL | 生成器 | 对应 | 来袭弹控制量(对应 | 3 层全连接隐藏层,每层 128 个神经元 | |
| 判别器 | 状态量(相对位置、速度矢量)与控制量拼接的向量 | 单元素判别值(用于区分生成器轨迹与专家轨迹),同时为生成器提供奖励信号 | 3 层全连接隐藏层,每层 128 个神经元 | ||
| LSTM-Transformer | 编码器 | 50 帧含来袭弹位置、速度的历史序列 | 输入序列的上下文特征向量 | 2层LSTM 层,每层128个神经元 | |
| 解码器 | 编码器输出的上下文特征向量 | 下一时刻来袭弹状态的中间预测特征 | 2层标准Transformer解码器,每层含8头自注意力子层(每个注意力头维度16),其他隐层维度128 | 采取因果掩码自注意力机制(保证自回归特性) | |
| 输出层 | 解码器输出的中间预测特征 | 下一时刻来袭弹三轴位置、速度(共6个输出维度) | 1 层全连接层,输出大小为 6 | 多步预测时采用滚动方式(引入上一时刻网络输出作为输入) |
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