正版 基于滑模理论的航空动力系统故障诊断与容错控制 肖玲斐//林

Chapter 1 Introduction
1.1 Fault Diagnosis and Fault Tolerant Control Theory
1.1.1 Faults Classification
1.1.2 Fault Diagnosis
1.1.3 Fault Tolerant Control
1.2 Sliding Mode Theory
1.2.1 Sliding Mode Control
1.2.2 Sliding Mode Observer
1.3 Fault Diagnosis and Fault Tolerant Control Based on Sliding Mode
1.3.1 Fault Diagnosis Based on Sliding Mode Observer
1.3.2 Sliding Mode Fault Tolerant Control
1.4 Fault Diagnosis and Fault Tolerant Control in Aircraft Power Systems
1.4.1 Sliding Mode Fault Diagnosis in Aircraft Power Systems
1.4.2 Sliding Mode Fault Tolerant Control in Aircraft Power Systems
1.5 Structure of This Book
Chapter 2 Aircraft Engine Sensor Faults Diagnosis Based on Sliding Mode Observer by Using Residual
2.1 Aircraft Engine Mathematical Model
2.1.1 Aircraft Engine Linear Model
2.1.2 Establishment of Aircraft Engine State Space Variable Model Based on Least Square Fitting
2.2 Mathematical Model of Sensor Fault in Aircraft Engine
2.3 Fault Diagnosis Method Based on Residual Error
2.3.1 System Model with Sensor Faults
2.3.2 Observer Design and Stability Analysis
2.3.3 Parameter Solution of Sliding Mode Observer Based on Linear Matrix Inequality
2.3.4 Sensor Fault Detection Based on Sliding Mode Observer
2.4 Simulation
2.5 Conclusions
Chapter 3 Multi-sensors Fault Diagnosis of Aircraft Engine Based on Kalman Filter Group
3.1 Introduction
3.2 Aircraft Engine Model
3.3 Design of Sensor Fault Diagnosis System for Aircraft Engine
3.3.1 Single Sensor Fault Diagnosis
3.3.2 Multi-sensors Fault Diagnosis
3.4 Simulation
3.5 Conclusions
Chapter 4 Fault Identification for Turboshaft Engines Based on Fractional-order Sliding Mode Observer
4.1 Introduction
4.2 Turboshaft Engine Linearized Model
4.3 Fault Identification Based on Fractional-order Sliding Mode Observer
4.4 Simulation
4.5 Conclusions
Chapter 5 Robust Fault Identification of Turbofan Engine Sensors Based on Fractional-order Integral Sliding Mode Observer
5.1 Introduction
5.2 Equilibrium Manifold Expansion Model of Turbofan Engine
5.3 Fractional-order Integral Sliding Mode Observer for Fault Identification
5.3.1 Preliminaries of Fractional-order Calculus
5.3.2 Design of Fractional-order Integral Sliding Mode Observer
5.4 Simulation
5.5 Conclusions
Chapter 6 Aireraft Engine Gas Path Fault Diagnosis Based on HPSO-TWSVM
6.1 Introduction
6.2 A Description of Aircraft Engine Gas Path Fault Diagnosis
6.3 Basic Principle of TWSVM
6.4 Algorithm of TWSVM Based on HPSO-TWSVM
6.4.1 Characters and Principle of HPSO
6.4.2 Selection of Kernel Function
6.4.3 Training Algorithm of TWSVM
6.5 Gas Path Fault Diagnosis Based on HPSO-TWSVM
6.5.1 Review of Gas Path Fault Diagnosis Based on HPSO-TWSVM
6.5.2 Procedure of Gas Path Fault Diagnosis Based on HPSO-TWSVM
6.6 Simulation
6.7 Conclusions
Chapter 7 Fault Reconstruction of Actuator in Aircraft Engine Based on Equilibrium Manifold Expansion Model and Sliding Mode
Observer
7.1 Introduction
7.2 Fault Reconfiguration of Actuator
7.3 Simulation
7.4 Conclusions
Chapter 8 Sliding Mode Control for Aircraft Engine Based on Genetic Algorithm
8.1 Basic Principle of Sliding Mode Control
8.1.1 Definition of Sliding Mode
8.1.2 Definition of Sliding Mode Variable Structure Control
8.1.3 Chattering Problem of Sliding Mode Variable Structure
8.1.4 Existence and Arrival Conditions of Sliding Mode
8.1.5 Equivalent Control and Sliding Mode
8.1.6 Basic Design Method of Sliding Mode Controller
8.1.7 Quasi-sliding Mode Control
8.2 Aircraft Engine Sliding Mode Control Based on Reaching Law
8.2.1 Sliding Mode Control Based on Exponential Reaching Law
8.2.2 Position Tracking Based on Exponential Reaching Law
8.3 Sliding Mode Control Based on Genetic Algorithm
8.3.1 Design of Sliding Mode Controller
8.3.2 Sliding Mode Controller Based on Genetic Algorithm
8.3.3 Simulation
8.4 Conclusions
Chapter 9 Aircraft Engine Sliding Mode Control Based on Variable Parameter Model
9.1 Overview of Variable Parameter Model in Envelope Range
9.2 Variable Parameter Model Based on BP Neural Network
9.3 Design of Sliding Mode Variable Structure Multivariable Control System
9.3.1 Requirements
9.3.2 Design Method of Sliding Mode Surface for Sliding Mode Control of Multivariable Systems
9.3.3 Sliding Mode Analysis of Sliding Mode Control for Multivariable System
9.4 Analysis of Reaching Law Based on Proportional-constant-variable Rate
9.5 Analysis of Reaching Law Based on PID
9.6 Simulation
9.7 Conclusions
Chapter 10 Integral Tangent Adaptive Fuzzy Sliding Mode Control for Aircraft Engine
10.1 Introduction
10.2 Design of Integral Fuzzy Adaptive Sliding Mode Controller for Aircraft Engine
10.2.1 Aircraft Engine Control System Model
10.2.2 Design of Hyperbolic Tangent Integral Sliding Surface
10.2.3 Design of Fuzzy Power Exponent Reaching Law
10.2.4 Design of Adaptive Fuzzy Sliding Mode Controller of Aircraft Engine
10.3 Simulation
10.4 Conclusions
Chapter 11 Aircraft Engine Nonlinear Sliding Mode Control Based on Artificial Bee Colony Algorithm
1l.1 Introduction
11.2 Preliminaries
11.2.1 Exact Linearization Theory
11.2.2 Artificial Bee Colony Algorithm
11.3 ABC-based Aircraft Engine Nonlinear Sliding Mode Controller Design
11.4 Simulation
11.5 Conclusions
Chapter 12 Robust Control for Electric Fuel Pump with Variant Nonlinear Loads Based on a New Combined Sliding Mode Surface
12.1 Introduction
12.2 System Configuration
12.3 Design of Combined Sliding Mode Controller
12.3.1 Controller Structure
12.3.2 Analysis of Linear Sliding Mode
12.3.3 Analysis of Quadratic Integral Sliding Mode
12.3.4 Design of Combined Sliding Mode Control Law
12.4 Stability of Closed-loop System
12.4.1 Reachability of Combined Sliding Mode Surface
12.4.2 Stability of the Closed-loop System in Sliding Mode
12.5 Simulation
12.6 Conclusions
Chapter 13 Aircraft Engine Sliding Mode Fault Tolerant Control Based on Sliding Mode Observer
13.1 Robust Reconstruction of Sensor Faults Based on Sliding Mode Observer
13.1.1 Robust Reconstruction of Sensor Faults
13.1.2 Simulation
13.2 Design of Integral Tangent Adaptive Fuzzy Sliding Mode Fault Tolerant Control System for Aircraft Engine
13.3 Simulation
13.4 Conclusions
Chapter 14 Aircraft Engine Sliding Mode Fault Tolerant Control Based on Kalman Filter
14.1 Design of Aircraft Engine Sliding Mode Tracking Controller
14.1 .1 Problem Description
14.1.2 Model Augmentation
14.1.3 Design of Sliding Surface
14.1.4 Design of Sliding Mode Control Law
14.1.5 Stability Analysis
14.2 Design of Aircraft Engine Sliding Mode Fault Tolerant Control
14.3 Simulation
14.4 Conclusions
Chapter 15 Sliding Mode Fault Tolerant Control for Aircraft Engine with Sensor Fault Based on PID Reaching Law
15.1 Introduction
15.2 Reconstruction of Sensor Fault Signal
15.3 System Description
15.4 Sliding Mode Fault Tolerant Controller Design for Sensor Fault
15.5 Simulation
15.5.1 Signal Reconstruction
15.5.2 PID Fault Tolerant Controller for Sensor Fault
15.5.3 H∞ Fault Tolerant Controller for Sensor Fault
15.5.4 Sliding Mode Fault Tolerant Controller for Sensor Fault
15.6 Conclusions
Chapter 16 Adaptive Fault Tolerant Control for Aircraft Engine with Sensors and Actuators Faults
16.1 Introduction
16.2 Design of Adaptive Fault Tolerant Controller
16.2.1 Engine Model
16.2.2 Adaptive Observer for Fault Diagnosis… ……… … … 217
16.2.3 Fault Tolerant Control Design
16.3 Simulation
16.4 Conclusions
Chapter 17 Sliding Mode Fault Tolerant Control for Aircraft Electric Fuel Pump with Actuator Fault
17.1 Fault Tolerant Controller Based on Walcott-Zak Observer
17.1.1 Design of Fault Tolerant Control System
17.1.2 Simulation
17.2 Fault Tolerant Controller Based on Hybrid Nonsingular Fast Terminal Sliding Mode Observer
17.2.1 Design of Fault Tolerant Control System
17.2.2 Simulation
17.3 Conclusions
Chapter 18 Guaranteed Cost Control and Fault Tolerant for STOVL Aircraft Engine
18.1 Introduction
18.2 Controller Design and Fault Tolerant Method
18.2.1 Problem Description
18.2.2 Guaranteed Cost Controller Design
18.2.3 Fault Tolerant Control Based on Kalman Filter
18.3 Simulation
18.4 Conclusions
Chapter 19 Robust Fault Tolerant Control Based on Sliding Mode for Aircraft Engines
19.1 Introduction
19.2 Mathematical Model of Aircraft Engine Control Systems
19.3 Main Results
19.3.1 Detection Observer Design
19.3.2 Adaptive Diagnostic Observer Design
19.3.3 Sliding Mode Fault Tolerant Control
19.3.4 Robust Stabilization Analysis
19.4 Simulation
19.5 Conclusions
References

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。