覃道亮｜北京航空航天大学｜学者主页

2018

Withdrawal: An Embedded Hardware-in-the-Loop Testbed for Aeroengine Simulation Education

Wei Ji, Daoliang Tan, Emmanuel Ndagijimana, Xi Wang

AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC)

DOI

2018

An Embedded Hardware-in-the-Loop Testbed for Aeroengine Simulation Education

Wei Ji, Daoliang Tan, Emmanuel Ndagijimana, Xi Wang

AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC)

DOI

2017

A Comparative Study of LPV Modeling for Turbofan Engines

Zhenhua Tian, Daoliang Tan, Xi Wang

AIAA/SAE/ASEE Joint Propulsion Conference (JPC)

DOI

2016

用于涡轴发动机传感器故障诊断的未知输入观测器干扰矩阵估算

杨超，王曦，时瑞军，周剑波，高世煌，覃道亮

《航空动力学报》

2015

Integrated Fault Estimation and Fault Tolerant Control: A Joint Design

Daoliang Tan, Ron J. Patton

IFAC-PapersOnLine

DOI

2015

A Relaxed Solution to Unknown Input Observers for State and Fault Estimation

Daoliang Tan, Ron J. Patton, Xi Wang

IFAC-PapersOnLine

DOI

2013

Linear-Matrix-Inequality-Based Fault Diagnosis for Gas Turbofan Engine Using Eigenstructure Assignment Principle

Yue Liu, Daoliang Tan, Bin Wang, Xi Wang

Applied Mechanics and Materials

DOI

2013

An extrapolation approach for aeroengine’s transient control law design

Xiangxing Kong, Xi Wang, Daoliang Tan, Ai He, Yue Liu

Chinese Journal of Aeronautics

DOI

2012

基于UIO的航空发动机执行机构故障诊断

何皑，覃道亮，孔祥兴，王曦

《推进技术》

2012

Unified Diagnostic Filtering for Turbofan Engine Control Systems Based on Matrix Pencil Observers

Daoliang Tan, Yue Liu, Ai He, Yun Liu, Xiangxing Kong, Xi Wang

DOI

2011

基于UIO的航空发动机控制系统传感器故障诊断

覃道亮，何皑，孔祥兴，王曦

《航空动力学报》

2011

An LMI-Based Anti-Windup Design for Acceleration and Deceleration Control of Jet Engines Using the H2/H? Optimization

He Ai, Daoliang Tan, Xi Wang

AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC)

DOI

2011

A Non-Iterative Aeroengine Model Based on Volume Effect

Xiangxing Kong, Xi Wang, Daoliang Tan, Ai He

AIAA Modeling and Simulation Technologies Conference

DOI

2011

Integration of Unknown Input Observers and Classification for Turbofan Engine Diagnosis

Daoliang Tan, Ai He, Xiangxing Kong, Xi Wang

DOI

2010

Evaluation of the LMI-Based Multivariable PID Controller Design for Turbo Aeroengines

Ai He, Daoliang Tan, Xi Wang, Lei Wang

Volume 3: Controls, Diagnostics and Instrumentation; Cycle Innovations; Marine

DOI

2010

Multivariable Aeroengine PID Control With Amplitude Saturation: An LMI Solution

Daoliang Tan, Ai He, Xi Wang, Yun Liu

Volume 3: Controls, Diagnostics and Instrumentation; Cycle Innovations; Marine

DOI

2008

Static Output Feedback-Based PI Control for Aeroengines Using Linear Matrix Inequality

Xi Wang, Yongxia Sun, Tiejun Zheng, Daoliang Tan

AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (JPC)

DOI

2005

Turbofan Engine Robust H-∞ Dynamical Output Feedback Control Design Based on LMI Method

Xi Wang, Daoliang Tan, Tiejun Zheng

DOI

覃道亮

精选作品

期刊论文

Withdrawal: An Embedded Hardware-in-the-Loop Testbed for Aeroengine Simulation Education

An Embedded Hardware-in-the-Loop Testbed for Aeroengine Simulation Education

A Comparative Study of LPV Modeling for Turbofan Engines

用于涡轴发动机传感器故障诊断的未知输入观测器干扰矩阵估算

Integrated Fault Estimation and Fault Tolerant Control: A Joint Design

A Relaxed Solution to Unknown Input Observers for State and Fault Estimation

Linear-Matrix-Inequality-Based Fault Diagnosis for Gas Turbofan Engine Using Eigenstructure Assignment Principle

An extrapolation approach for aeroengine’s transient control law design

基于UIO的航空发动机执行机构故障诊断

Unified Diagnostic Filtering for Turbofan Engine Control Systems Based on Matrix Pencil Observers

基于UIO的航空发动机控制系统传感器故障诊断

An LMI-Based Anti-Windup Design for Acceleration and Deceleration Control of Jet Engines Using the H2/H? Optimization

A Non-Iterative Aeroengine Model Based on Volume Effect

Integration of Unknown Input Observers and Classification for Turbofan Engine Diagnosis

Evaluation of the LMI-Based Multivariable PID Controller Design for Turbo Aeroengines

Multivariable Aeroengine PID Control With Amplitude Saturation: An LMI Solution

Static Output Feedback-Based PI Control for Aeroengines Using Linear Matrix Inequality

Turbofan Engine Robust H-∞ Dynamical Output Feedback Control Design Based on LMI Method

研究方向