Feng Lu
Orcid: 0000-0002-6620-2399Affiliations:
- Nanjing University of Aeronautics and Astronautics, Jiangsu Province Key Laboratory of Aerospace Power Systems, China (PhD 2009)
According to our database1,
Feng Lu
authored at least 12 papers
between 2012 and 2025.
Collaborative distances:
Collaborative distances:
Timeline
Legend:
Book In proceedings Article PhD thesis Dataset OtherLinks
Online presence:
-
on orcid.org
On csauthors.net:
Bibliography
2025
A Multivariable Performance Recovery Control Method for Turboprop Engine Based on Data Prediction Model.
IEEE Trans. Aerosp. Electron. Syst., August, 2025
An Online Gas Path Fault Diagnosis for Aircraft Engine Transient Behavior Using iB-EKF Algorithm.
IEEE Trans. Aerosp. Electron. Syst., April, 2025
2024
IEEE Trans. Aerosp. Electron. Syst., December, 2024
Anomaly Detection Method for Rocket Engines Based on Convex Optimized Information Fusion.
Sensors, January, 2024
2020
Restricted-Boltzmann-Based Extreme Learning Machine for Gas Path Fault Diagnosis of Turbofan Engine.
IEEE Trans. Ind. Informatics, 2020
2018
Parsimonious Kernel Recursive Least Squares Algorithm for Aero-Engine Health Diagnosis.
IEEE Access, 2018
Aero Engine Gas Path Performance Tracking Based on Multi-Sensor Asynchronous Integration Filtering Approach.
IEEE Access, 2018
A Hybrid Kalman Filtering Approach Based on Federated Framework for Gas Turbine Engine Health Monitoring.
IEEE Access, 2018
2017
Robust In-Flight Sensor Fault Diagnostics for Aircraft Engine Based on Sliding Mode Observers.
Sensors, 2017
2016
Recursive reduced kernel based extreme learning machine for aero-engine fault pattern recognition.
Neurocomputing, 2016
2013
Multivariable PID parameters tuning method based on model matching on frequency domain for aero-engine.
Proceedings of the 2013 IEEE/ASME International Conference on Advanced Intelligent Mechatronics, 2013
2012
Fault Diagnostics for Turbo-Shaft Engine Sensors Based on a Simplified On-Board Model.
Sensors, 2012