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Fault Diagnosis and Fault Tolerant Control of Aerospace Powe
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商品名称: | Fault Diagnosis and Fault Tolerant Control of Aerospace Power Systems Based on Sliding Mode Theory 基于滑模理论的航空动 | 开本: | 16开 |
作者: | 肖玲斐 林聪 著 | 定价: | 79.00 |
ISBN号: | 9787512436282 | 出版时间: | 2022-03-01 |
出版社: | 北京航空航天大学出版社 | 印刷时间: | 2022-03-01 |
版次: | 1 | 印次: | 1 |
Chapter 1 Introduction 1
1.1 Fault Diagnosis and Fault Tolerant Control Theory 1
1.1.1 Faults Classification 1
1.1.2 Fault Diagnosis 5
1.1.3 Fault Tolerant Control 7
1.2 Sliding Mode Theory 11
1.2.1 Sliding Mode Control 11
1.2.2 Sliding Mode Observer 12
1.3 Fault Diagnosis and Fault Tolerant Control Based on Sliding Mode 13
1.3.1 Fault Diagnosis Based on Sliding Mode Observer 13
1.3.2 Sliding Mode Fault Tolerant Control 14
1.4 Fault Diagnosis and Fault Tolerant Control in Aircraft Power Systems 15
1.4.1 Sliding Mode Fault Diagnosis in Aircraft Power Systems 15
1.4.2 Sliding Mode Fault Tolerant Control in Aircraft Power Systems 16
1.5 Structure of This Book 16
Chapter 2 Aircraft Engine Sensor Faults Diagnosis Based on Sliding Mode Observer by Using Residual 18
2.1 Aircraft Engine Mathematical Model 18
2.1.1 Aircraft Engine Linear Model 18
2.1.2 Establishment of Aircraft Engine State Space Variable Model Based on Least Square Fitting 21
2.2 Mathematical Model of Sensor Fault in Aircraft Engine 23
2.3 Fault Diagnosis Method Based on Residual Error 23
2.3.1 System Model with Sensor Faults 24
2.3.2 Observer Design and Stability Analysis 24
2.3.3 Parameter Solution of Sliding Mode Observer Based on Linear Matrix Inequality 25
2.3.4 Sensor Fault Detection Based on Sliding Mode Observer 27
2.4 Simulation 28
2.5 Conclusions 31
Chapter 3 Multi-sensors Fault Diagnosis of Aircraft Engine Based on Kalman Filter Group 32
3.1 Introduction 32
3.2 Aircraft Engine Model 33
3.3 Design of Sensor Fault Diagnosis System for Aircraft Engine 35
3.3.1 Single Sensor Fault Diagnosis 35
3.3.2 Multi-sensors Fault Diagnosis 36
3.4 Simulation 37
3.5 Conclusions 46
Chapter 4 Fault Identification for Turboshaft Engines Based on Fractional-order Sliding Mode Observer 47
4.1 Introduction 47
4.2 Turboshaft Engine Linearized Model 48
4.3 Fault Identification Based on Fractional-order Sliding Mode Observer 49
4.4 Simulation 51
4.5 Conclusions 55
Chapter 5 Robust Fault Identification of Turbofan Engine Sensors Based on Fractional-order Integral Sliding Mode Observer 56
5.1 Introduction 56
5.2 Equilibrium Manifold Expansion Model of Turbofan Engine 57
5.3 Fractional-order Integral Sliding Mode Observer for Fault Identification 58
5.3.1 Preliminaries of Fractional-order Calculus 58
5.3.2 Design of Fractional-order Integral Sliding Mode Observer 59
5.4 Simulation 64
5.5 Conclusions 70
Chapter 6 Aircraft Engine Gas Path Fault Diagnosis Based on HPSO-TWSVM 71
6.1 Introduction 71
6.2 A Description of Aircraft Engine Gas Path Fault Diagnosis 71
6.3 Basic Principle of TWSVM 73
6.4 Algorithm of TWSVM Based on HPSO-TWSVM 74
6.4.1 Characters and Principle of HPSO 74
6.4.2 Selection of Kernel Function 77
6.4.3 Training Algorithm of TWSVM 78
6.5 Gas Path Fault Diagnosis Based on HPSO-TWSVM 79
6.5.1 Review of Gas Path Fault Diagnosis Based on HPSO-TWSVM 79
6.5.2 Procedure of Gas Path Fault Diagnosis Based on HPSO-TWSVM 80
6.6 Simulation 82
6.7 Conclusions 84
Chapter 7 Fault Reconstruction of Actuator in Aircraft Engine Based on Equilibrium Manifold Expansion Model and Sliding Mode Observer 85
7.1 Introduction 85
7.2 Fault Reconfiguration of Actuator 86
7.3 Simulation 87
7.4 Conclusions 88
Chapter 8 Slidin......
In the field of aerospace power systems, there are few books on fault diagnosis and fault tolerant control based on sliding mode theory. On the basis of authors many years of technical research and the results of many scientific research projects, this book comprehensively expounds the key theories and main methods of fault diagnosis and fault tolerant control of aerospace power systems based on sliding mode theory. Several design methods for sliding mode observers and sliding mode controllers are introduced, and are utilized to realize fault diagnosis and fault tolerant control for some typical aerospace power systems. This book has remarkable characteristics of combining theory with engineering.Except the Chapter 1 which is the introduction, there are three parts in this book. The first part is about fault diagnosis methods for aerospace power systems, which includes six chapters. The second part includes five chapters and different sliding mode control methods for aerospace power systems are given. The third part is comprised of the remaining seven chapters, in which several fault tolerant control methods for aerospace
power systems are discussed.
This book can be used as reference book for scientific researchers, engineering technicians, teachers and senior undergraduates, masters and doctoral students, who are in the field of aerospace, automation, power machinery and engineering, specially enengaged in the research and application of system modeling,control,fault diagnosis, fault tolerance,etc.
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