蕾蕾 邓

Ms. 蕾蕾 邓

orcid

Research Focus & Metrics

Academic Career Length

4Years (2023-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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27 May 2025 in Aerospace
Verified
Journal Article
Open access
PDF file
RLRuihan Liang
Ruihan Liang
WPWeijun Pan
Weijun Pan
QZQinghai Zuo
Qinghai Zuo
CZChen Zhang
Chen Zhang
SCShenhao Chen
Shenhao Chen
蕾邓蕾蕾 邓
蕾蕾 邓
As a forward-looking development in air traffic control (ATC), remote towers rely on virtualized information presentation, which may exacerbate visual fatigue among controllers and compromise operational safety. This study proposes a visual fatigue recognition model based on multimodal physiological signals. A 60-min simulated remote tower task was conducted with 36 participants, during which eye-tracking (ET), electroencephalography (EEG), electrocardiography (ECG), and electrodermal activity (EDA) signals were collected. Subjective fatigue questionnaires and objective ophthalmic measurements were also recorded before and after the task. Statistically significant features were identified through paired t-tests, and fatigue labels were constructed by combining subjective and objective indicators. LightGBM was then employed to rank feature importance by integrating split frequency and information gain into a composite score. The top 12 features were selected and used to train a multilayer perceptron (MLP) for classification. The model achieved an average balanced accuracy of 0.92 and an F1 score of 0.90 under 12-fold cross-validation, demonstrating excellent predictive performance. The high-ranking features spanned four modalities, revealing typical physiological patterns of visual fatigue across ocular behavior, cortical activity, autonomic regulation, and arousal level. These findings validate the effectiveness of multimodal fusion in modeling visual fatigue and provide theoretical and technical support for human factor monitoring and risk mitigation in remote tower environments.

19 June 2024 in Aerospace
Verified
Journal Article
Open access
PDF file
蕾邓蕾蕾 邓
蕾蕾 邓
WPWeijun Pan
Weijun Pan
YWYuhao Wang
Yuhao Wang
TLTIAN LUAN
TIAN LUAN
YLYuanfei Leng
Yuanfei Leng
To overcome the time-consuming drawbacks of Computational Fluid Dynamics (CFD) numerical simulations, this paper proposes a hybrid model named PA-TLA (parallel architecture combining a TCN, LSTM, and an attention mechanism) based on the concept of intelligent aerodynamics and a parallel architecture. This model utilizes CFD data to drive efficient predictions of aircraft wake evolution at different initial altitudes during the approach phase. Initially, CFD simulations of continuous initial altitudes during the approach phase are used to generate aircraft wake evolution data, which are then validated against real-world LIDAR data to verify their reliability. The PA-TLA model is designed based on a parallel architecture, combining Long Short-Term Memory (LSTM) networks, Temporal Convolutional Networks (TCNs), and a tensor concatenation module based on the attention mechanism, which ensures computational efficiency while fully leveraging the advantages of each component in a parallel processing framework. The study results show that the PA-TLA model outperforms both the LSTM and TCN models in predicting the three characteristic parameters of aircraft wake: vorticity, circulation, and Q-criterion. Compared to the serially structured TCN-LSTM, PA-TLA achieves an average reduction in mean squared error (MSE) of 6.80%, in mean absolute error (MAE) of 7.70%, and in root mean square error (RMSE) of 4.47%, with an average increase in the coefficient of determination (R2) of 0.36% and a 35% improvement in prediction efficiency. Lastly, this study combines numerical simulations and the PA-TLA deep learning architecture to analyze the near-ground wake vortex evolution. The results indicate that the ground effect increases air resistance and turbulence as vortices approach the ground, thereby slowing the decay rate of the wake vortex strength at lower altitudes. The ground effect also accelerates the dissipation and movement of vortex centers, causing more pronounced changes in vortex spacing at lower altitudes. Additionally, the vortex center height at lower altitudes initially decreases and then increases, unlike the continuous decrease observed at higher altitudes.

15 July 2025 in IEEE Transactions on Aerospace and Electronic Systems
Verified
Journal Article
Open access
蕾邓蕾蕾 邓
蕾蕾 邓
WPWeijun Pan
Weijun Pan
PZPeng Zhao
Peng Zhao
KCKuanming Chen
Kuanming Chen
XWXuan Wang
Xuan Wang
With the rapid development of the aviation industry, airspace environments have become increasingly complex. In addition, fixed-distance wake separation standards, which are constrained by overly conservative spacing intervals and limited adaptability to dynamic conditions, can no longer meet mod ern operational demands. Therefore, how to perform real-time detection of wake-vortex data using the Doppler LiDAR and achieve dynamic wake-separation reductions has become a crucial challenge in improving airport operational efficiency. To this end, this paper proposes a two-branch co-learning framework named the TransCNN model, which combines convolutional neural networks (CNNs) and Transformers to align multi-dimensional learning tasks. The proposed framework includes a multi-scale hybrid attention convolution module that enhances the local feature extraction effect in CNN branches. In addition, it includes a global feature fusion module that integrates global information obtained from transformer branches into CNN feature maps. The proposed framework is verified using wake-vortex data obtained by Doppler LiDAR in the approach areas of Qingdao Jiaodong International Airport. The experimental results demonstrate that the proposed TransCNN model excels in LiDAR-based wake-vortex identification, achieving an accuracy of 99.09%, which represents a 12.09% improvement over traditional support vector machine methods. Further, the variation patterns of the wake-vortex dissipation time under different wind field conditions are analyzed, and the superior performance of the TransCNN model in enhancing flight safety and operational efficiency is validated through Markov chain Monte Carlo simulations

13 May 2024 in Preprints.org
Verified
Preprint
Open access
PDF file
蕾邓蕾蕾 邓
蕾蕾 邓
WPWeijun Pan
Weijun Pan
YWYuhao Wang
Yuhao Wang
TLTIAN LUAN
TIAN LUAN
YLYuanfei Leng
Yuanfei Leng
To overcome the time-consuming drawbacks of Computational Fluid Dynamics (CFD) numerical simulations, this paper proposes a hybrid model based on a parallel architecture based on the concept of intelligent aerodynamics, named PA-TLA (Parallel Architecture combining TCN, LSTM, and Attention mechanism). This model utilizes CFD data to drive efficient predictions of aircraft wake evolution at different initial altitudes during the approach phase. Initially, CFD simulations of continuous initial altitudes during the approach phase are used to generate aircraft wake evolution data, which are then validated against real-world LIDAR data to verify their reliability. The PA-TLA model is designed based on a parallel architecture, combining Long Short-Term Memory networks (LSTM), Temporal Convolutional Networks (TCN), and a tensor concatenation module based on the attention mechanism, which ensures computational efficiency while fully leveraging the advantages of each component in a parallel processing framework. The study results show that the PA-TLA model outperforms both the LSTM and TCN models in predicting the three characteristic parameters of aircraft wake: vorticity, circulation, and Q-criterion. Compared to the serially structured TCN-LSTM, PA-TLA achieves an average reduction in mean squared error (MSE) by 6.80%, mean absolute error (MAE) by 7.70%, and root mean square error (RMSE) by 4.47%, with an average increase in the coefficient of determination (R²) by 0.36%, and a 35% improvement in prediction efficiency. Lastly, this study combines numerical simulation and the PA-TLA deep learning architecture to analyze the characteristics of wake evolution during the near-ground phase, providing theoretical value for further reducing aircraft wake intervals and enhancing airport operational efficiency.

4 May 2025 in Sensors
Verified
Journal Article
Open access
PDF file
WPWeijun Pan
Weijun Pan
WYWang Yuhao
Wang Yuhao
蕾邓蕾蕾 邓
蕾蕾 邓
YJYanqiang Jiang
Yanqiang Jiang
YLYuan-Fei Leng
Yuan-Fei Leng
This paper proposes a hybrid deep learning network architecture (Inception-VGG16) to address the challenge of accurate aircraft wake vortex identification. The model first employs a Feature0 module for preliminary feature extraction of two-dimensional Doppler radar radial velocity data. This module comprises convolution, batch normalization, ReLU activation, and max pooling operations. Subsequently, improved InceptionB and InceptionC modules are utilized for parallel extraction of multi-scale features. The InceptionB former module adopts two parallel branches, combining 1 × 1 and 3 × 3 convolutions, and outputting 64-channel feature maps, while the InceptionC latter module expands the number of channels number to 128, enhancing the model’s feature representation capability. The backend employs the VGG16’s hierarchical structure, performing deep feature extraction through multiple convolution and pooling operations, and ultimately achieving wake vortex classification through fully connected layers. Experimental validation based on 3530 wind field samples collected at the Chengdu Shuangliu Airport demonstrates that compared to traditional methods (SVM, KNN, RF) and single deep networks (VGG16), the proposed hybrid model achieves a classification accuracy of 98.8%, significantly outperforming comparative traditional methods (SVM, KNN, RF) and single deep networks (VGG16). The model not only overcomes the limitations of single networks in processing multi-scale wake features but also enhances the model’s ability to identify wake vortices in complex backgrounds through deep feature hierarchies, providing a new technical solution for aviation safety monitoring systems based on deep learning.

11 October 2024 in Aerospace
Verified
Journal Article
Open access
PDF file
蕾邓蕾蕾 邓
蕾蕾 邓
WPWeijun Pan
Weijun Pan
TLTIAN LUAN
TIAN LUAN
CZChen Zhang
Chen Zhang
YLYuanfei Leng
Yuanfei Leng
Wake vortices generated by aircraft during near-ground operations have a significant impact on airport safety during takeoffs and landings. Identifying wake vortices in complex airspaces assists air traffic controllers in making informed decisions, ensuring the safety of aircraft operations at airports, and enhancing the intelligence level of air traffic control. Unlike traditional image recognition, identifying wake vortices using airborne LiDAR data demands a higher level of accuracy. This study proposes the IRSN-WAKE network by optimizing the Inception-ResNet-v2 network. To improve the model’s feature representation capability, we introduce the SE module into the Inception-ResNet-v2 network, which adaptively weights feature channels to enhance the network’s focus on key features. Additionally, we design and incorporate a noise suppression module to mitigate noise and enhance the robustness of feature extraction. Ablation experiments demonstrate that the introduction of the noise suppression module and the SE module significantly improves the performance of the IRSN-WAKE network in wake vortex identification tasks, achieving an accuracy rate of 98.60%. Comparative experimental results indicate that the IRSN-WAKE network has higher recognition accuracy and robustness compared to common recognition networks, achieving high-accuracy aircraft wake vortex identification and providing technical support for the safe operation of flights.