基本情况

鲁峰，工学博士，南京航空航天大学教授。现为中国空天动力联合会发动机控制技术专业委员会委员，国家先进航空发动机协同创新中心适航组成员，中国（南京）知识产权保护中心技术专家，国家自然科学基金函评专家，教育部研究生学位论文评审专家。先后主持国家自然科学基金2项，国家科技重大专项专题、国防173子课题，以及其他基金、国防预研等项目20余项，获得教育部科技进步二等奖、国防科技进步二等奖，获江苏省“青蓝工程”优秀青年骨干教师。在国内外期刊和会议上发表学术论文百余篇，SCI论文近50篇，申请国家发明专利30余项，授权16项，软件著作权4项，译著1部。


研究领域

推进系统建模与控制、信号处理、测试与诊断


论文发表

  1. Xin Zhou, Wenjuan Chen, Jinquan Huang, Jingtian Liu, Feng Lu, A thrust estimation and control method of an adaptive cycle engine based on improved MFAC algorithm, Chinese Journal of Aeronautics, 2025, 38(5), 103424.
  2. Zelong Zou, Xin Zhou, Jinquan Huang, Wenlong Jiang, Feng Lu, An online gas path fault diagnosis for aircraft engine transient behavior using iB-EKF algorithm, IEEE Transactions on Aerospace and Electronic Systems, 2025, 61(2), 2659-2678.
  3. Xinhao Han, Xin Zhou, Feng Lu, Jinquan Huang, Data model-based sensor fault diagnosis algorithm for closed-loop control systems, Measurement, 2025, 246(31), 116715.
  4. Yingchen Guo, Jiazhu Teng, Xin Zhou, Zelong Zou, Jinquan Huang, Feng Lu, Real-time adaptive model of mainstream parameters for aircraft engines based on OSELM-EKF, Aerospace Science and Technology, 2024, 109662.
  5. Ansheng Ma, Xin Zhou, Zelong Zou, Jinquan Huang, Feng Lu, Thrust online fusion estimation of high-flow dual variable cycle engine, Aerospace Science and Technology, 2024, 152, 109388.
  6. Bingqiang Yu, Yi Peng, Jinquan Huang, Feng Lu, LSTM-Fuzzy logic for fault forecasting and mitigation in propulsion system, IEEE Transactions on Aerospace and Electronic Systems, 2024, 60(6), 8929-8944.
  7. Hao Sun, Yuehua Cheng, Bin Jiang, Feng Lu, Na Wang, Kim, Jongmyon, Anomaly detection method for rocket engine based on convex optimized information fusion, Sensors, 2024, 24(2), 415.
  8. Peng Jin, Xin Zhou, Feng Lu, Jinquan Huang, Haiqin Qin, Yahui Gao, A novel analytical redundancy method based on decision-level fusion for aero-engine sensors, Nonlinear Dynamics, 2023, 111, 13215-13234.
  9. Xin Zhou, Jinquan Huang, Feng Lu, Wenxiang Zhou, Pengfei Liu, A Novel Compound Fault-Tolerant Method Based on Online Sequential Extreme Learning Machine with Cycle Reservoir for Turbofan Engine Direct Thrust Control, Aerospace Science and Technology, 2023, 132, 108059.
  10. 唐杰; 鲁峰; 周文祥; 黄金泉; 进气道/发动机一体化多变量控制方法研究, 推进技术,2023, 44(1): 248-257.