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Fault Diagnosis and Fault Tolerant Control of Aerospace Power Systems Based on Sliding Mode Theory（ 
定 价：79 元
9 7 4 8 3 7 6 5 2 1 8 2 2 
本书较为全面地阐述了基于滑模理论航空动力系统故障诊断与容错控制的关键理论和主要方法，给出了典型航空动力系统的多种滑模鲁棒控制方法、滑模观测器设计方法、滑模容错控制方法的仿真实例，具有理论与工程相结合的显著特点。
本书可作为航空航天、自动化、动力机械和工程相关领域从事系统建模、控制、故障诊断、容错设计等研究与应用工作的科研人员、工程技术人员及高等院校相关专业的教师、高年级本科生、硕士生和博士生的参考书。
Aerospace power systems provide the thrust of forward movement and the necessary speed to lift off for aircrafts. The most important part in an aerospace power system is the aircraft engine. With the development of science and technology in various countries, people have higher and higher requirements on the control performance of aerospace power systems,which undoubtedly increases the control difficulty of aerospace power systems. Sliding mode theory includes sliding mode controller design method and sliding mode observer design method. Because of the good robustness and relatively simple strategy,sliding mode theory has attracted more and more attentions all around world from science researchers to engineering technicians. The control systems in modern aircraft engines are carried out by Full Authority Digital Electronic Control (FADEC) systems. The FADEC needs to work with the signal measured by the relevant sensors on the aircraft engine, which contains a large number of electronic components, sensors and actuators. Most of these components work in the working environment of high temperature, high pressure and alternating stress of aircraft engine, which makes them prone to failure and several faults occur frequently. Once serious faults occur, the consequence may be unimaginable. Therefore, fault diagnosis and fault tolerant control for aerospace power system is particularly important. In view of this, we write this book by summarizing years of scientific research results,focusing on the sliding mode theory for the fault diagnosis and fault tolerant control of aerospace power systems. Focussing on the fault diagnosis and fault tolerant control problems in aerospace power systems, this book introduces a variety of sliding mode observer design, sliding mode controller design and sliding mode fault tolerant control system construction methods.Correspondingly, except the Chapter 1, which is the introduction, there are three parts in this book. The first part includes six chapters, which discuss fault diagnosis of aerospace power systems. The second part includes five chapters and different sliding mode control methods are presented for aerospace power systems. The third part, which is comprised of seven chapters, shows several fault tolerant control methods for aerospace power systems. We sincerely thank our students and friends. Thank you for your help and support in writing this book. In the process of editing and publishing this book, many staff in Beihang University Press have worked hard, and we would like to express our gratitude here also. Limited to our ability, this book is inevitably inadequate or even wrong, and we urge readers, experts and scholars from all areas to criticize and correct us.
Xiao Lingfei and Lin Cong June 11,2021 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 。。。。。。 Chapter 7 Fault Reconstruction of Actuator in Aircraft Engine Based on Equilibrium Manifold Expansion Model and Sliding Mode Observer 85 。。。。。。 Chapter 8 Sliding Mode Control for Aircraft Engine Based on Genetic Algorithm 90 。。。。。。 Chapter 9 Aircraft Engine Sliding Mode Control Based on Variable Parameter Model 109 。。。。。。 Chapter 11 Aircraft Engine Nonlinear Sliding Mode Control Based on Artificial Bee Colony Algorithm 138 。。。。。。 Chapter 12 Robust Control for Electric Fuel Pump with Variant Nonlinear Loads Based on a New Combined Sliding Mode Surface 154 。。。。。。 Chapter 13 Aircraft Engine Sliding Mode Fault Tolerant Control Based on Sliding Mode Observer 173 13.1 Robust Reconstruction of Sensor Faults Based on Sliding Mode Observer 173 13.1.1 Robust Reconstruction of Sensor Faults 178 13.1.2 Simulation 181 13.2 Design of Integral Tangent Adaptive Fuzzy Sliding Mode Fault Tolerant Control System for Aircraft Engine 186 13.3 Simulation 187 13.4 Conclusions 191 Chapter 14 Aircraft Engine Sliding Mode Fault Tolerant Control Based on Kalman Filter 192 14.1 Design of Aircraft Engine Sliding Mode Tracking Controller 192 14.1.1 Problem Description 192 14.1.2 Model Augmentation 193 14.1.3 Design of Sliding Surface 193 14.1.4 Design of Sliding Mode Control Law 195 14.1.5 Stability Analysis 196 14.2 Design of Aircraft Engine Sliding Mode Fault Tolerant Control 197 14.3 Simulation 197 14.4 Conclusions 202 Chapter 15 Sliding Mode Fault Tolerant Control for Aircraft Engine with Sensor Fault Based on PID Reaching Law 203 15.1 Introduction 203 15.2 Reconstruction of Sensor Fault Signal 203 15.3 System Description 205 15.4 Sliding Mode Fault Tolerant Controller Design for Sensor Fault 206 15.5 Simulation 207 15.5.1 Signal Reconstruction 207 15.5.2 PID Fault Tolerant Controller for Sensor Fault 209 15.5.3 H ∞ Fault Tolerant Controller for Sensor Fault 211 15.5.4 Sliding Mode Fault Tolerant Controller for Sensor Fault 213 15.6 Conclusions 214 16.1 Introduction 216 16.2 Design of Adaptive Fault Tolerant Controller 217 16.2.1 Engine Model 217 16.2.2 Adaptive Observer for Fault Diagnosis 217 16.2.3 Fault Tolerant Control Design 219 16.3 Simulation 220 16.4 Conclusions 225 Chapter 17 Sliding Mode Fault Tolerant Control for Aircraft Electric Fuel Pump with Actuator Fault 226 17.1 Fault Tolerant Controller Based on Walcott Zak Observer 226 17.1.1 Design of Fault Tolerant Control System 226 17.1.2 Simulation 228 17.2 Fault Tolerant Controller Based on Hybrid Nonsingular Fast Terminal Sliding Mode Observer 231 17.2.1 Design of Fault Tolerant Control System 231 17.2.2 Simulation 234 17.3 Conclusions 238 18.1 Introduction 239 18.2 Controller Design and Fault Tolerant Method 240 18.2.1 Problem Description 240 18.2.2 Guaranteed Cost Controller Design 242 18.2.3 Fault Tolerant Control Based on Kalman Filter 247 18.3 Simulation 248 18.4 Conclusions 250 19.1 Introduction 252 19.2 Mathematical Model of Aircraft Engine Control Systems 253 19.3 Main Results 256 19.3.1 Detection Observer Design 256 19.3.2 Adaptive Diagnostic Observer Design 256 19.3.3 Sliding Mode Fault Tolerant Control 257 19.3.4 Robust Stabilization Analysis 258 19.4 Simulation 261 19.5 Conclusions 267 References 268
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