主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
融合注意力机制的航空发动机推力估计方法研究
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南京航空航天大学

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V239

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Research on Aircraft Engine Thrust Estimation Method Incorporating Attention Mechanism
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College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics

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    摘要:

    准确预测航空发动机推力大小对直接控制发动机推力具有重要意义。为了提升航空发动机推力估计模型的准确性和实用性,针对时间序列预测构建融合LSTM 和注意力机制的多任务LSTM-Attention 模型;针对不同飞行条件下推力估计的问题,运用Fine-tune 和改进DANN 的迁移学习方法以增强模型对于多工况条件下的适应性。结果表明:LSTM 融合注意力机制可以有效地对长时间序列数据进行建模,修正了LSTM 在全局建模能力上不足的问题,同时也克服了注意力机制难以捕捉相对位置信息的局限;多任务学习策略能显著提高模型在油门杆突变节点处的预测精度,进一步提高了模型的准确性;当目标域数据较少时应当选择Fine-tune,而在目标域数据充足的情况下使用改进DANN 方法将得到准确性更高的模型。

    Abstract:

    This study aims to enhance the accuracy and practicality of thrust estimation models for aero engines. The research first constructs a multi-task LSTM-Attention model that integrates Long Short-Term Memory (LSTM) and attention mechanisms for time series forecasting. Additionally, to address the issue of thrust estimation under different flight conditions, this paper employs Fine-tuning and an improved Domain-Adversarial Neural Network (DANN) transfer learning method to strengthen the model"s adaptability to multiple operational conditions. The results demonstrate that LSTM combined with the attention mechanism can effectively model long time series data, rectifying LSTM"s insufficiency in global modeling capabilities, while also overcoming the limitation of the attention mechanism in capturing relative position information. The multi-task learning strategy can significantly improve the model"s prediction accuracy at the abrupt changes in the throttle levers, further enhancing the model"s accuracy. The study of thrust prediction under different conditions based on transfer learning methods indicates that Fine-tuning should be selected when there is limited target domain data, while the modified DANN method will yield a model with higher accuracy when there is sufficient target domain data. This research provides a more accurate solution to the problem of thrust estimation for aero engines and has significant reference value for future research and practical applications.

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历史
  • 收稿日期:2023-09-12
  • 最后修改日期:2024-02-05
  • 录用日期:2024-02-22
  • 在线发布日期: 2024-09-29
  • 出版日期: