中国民航大学学报 ›› 2026, Vol. 44 ›› Issue (4): 34-41.doi: 10.27055/j.1674-5590.2026.04.006

• 未来机场及智能装备 • 上一篇    下一篇

飞机-跑道系统动力学响应的 LSTM 智能代理模型

  

  1. (同济大学a.道路与交通工程教育部重点实验室;b.民航飞行区设施耐久与运行安全重点实验室,上海 201804)
  • 收稿日期:2026-04-14 修回日期:2026-06-19 出版日期:2026-08-31 发布日期:2026-08-31
  • 通讯作者: 刘诗福
  • 作者简介:毛卫昱(2001— ),男,山东青岛人,硕士研究生,研究方向为道路与机场工程.
  • 基金资助:
    国家重点研发计划项目(2024YFB2605602);国家自然科学基金项目(52572380)

LSTM-based intelligent surrogate model for dynamic response of the aircraft-runway system

  1. (a. Key Laboratory of Road and Traffic Engineering, Ministry of Education; b. Key Laboratory of Infrastructure Durability and Operation Safety in Airfield of CAAC, Tongji University, Shanghai 201804, China)
  • Received:2026-04-14 Revised:2026-06-19 Online:2026-08-31 Published:2026-08-31
  • Contact: LIU Shifu

摘要: 为解决飞机-跑道系统动力学仿真主要依赖数值模型,导致计算效率偏低,难以满足智能跑道系统平台实 时响应需求的问题,本文提出基于长短期记忆网络(LSTM,long short-term memory)的飞机-跑道系统动力 学响应智能代理模型,以B737-800机型、济南遥墙国际机场跑道为研究对象,实现动力学响应快速精准 预测。基于扩展耦合动力学求解程序构建多工况数据集,设计双层LSTM架构并优化训练策略,以提升 模型泛化能力。结果表明,与传统数值仿真相比,平稳滑行工况下模型预测的平均相对误差低于3%;在 260 km/h 滑跑速度下,单次计算耗时由277.20 s缩至0.07 s,计算效率提升约3 960倍,且泛化性良好。该 模型为飞机-跑道系统动力学响应的实时精准分析提供了新的技术路径。

关键词: 飞机-跑道系统, 动力学响应, 长短期记忆网络(LSTM), 智能代理模型

Abstract: To solve the problem that the dynamic simulation of the aircraft-runway system mainly relies on numerical mod鄄 els, resulting in low computational efficiency and making it difficult to meet the real-time response requirements of the intelligent runway system platform, this paper proposes an intelligent surrogate model for the dynamic re鄄 sponse of the aircraft-runway system based on long short-term memory (LSTM). Taking the B737-800 aircraft and Jinan Yaoqiang International Airport runway as the research objects, the model achieves fast and accurate prediction of dynamic response. Based on the multi-condition dataset constructed by extending the coupled dy鄄 namics solver, a dual-layer LSTM architecture is designed and the training strategy is optimized to enhance the model′s generalization ability. The results show that, compared with the traditional numerical simulation, the av鄄 erage relative error of the model prediction under the steady taxiing condition is less than 3%; at a taxiing speed of 260 km/h, the computation time for a single run is reduced from 277.20 s to 0.07 s, and the computational effi鄄 ciency is improved by approximately 3 960 times, with good generalization performance. This model provides a new technical path for the real-time and accurate analysis of the dynamic response of the aircraft-runway system.

Key words: aircraft-runway system, dynamic response, long short-term memory (LSTM), intelligent surrogate model

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