Fault Diagnosis and Fault-Tolerant Control and Guidance for Aerospace Vehicles : From Theory to Application
By: Zolghadri, ali.
Contributor(s): Henry, David | Cieslak, Jérôme | Efimov, Denis | Goupil, Philippe.Material type: TextSeries: eBooks on Demand.Advances in Industrial Control: Publisher: Dordrecht : Springer, 2013Description: 1 online resource (227 p.).ISBN: 9781447153139.Subject(s): Fault location (Engineering)Genre/Form: Electronic books.Additional physical formats: Print version:: Fault Diagnosis and Fault-Tolerant Control and Guidance for Aerospace Vehicles : From Theory to ApplicationDDC classification: 629.11 | 629.8 Online resources: Click here to view this ebook.
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Series Editors' Foreword; Foreword; Preface; Contents; Chapter 1: Introduction; 1.1 Motivations; 1.2 Book Outline; Chapter 2: Review and Basic Concepts; 2.1 Introduction; 2.1.1 Fault Detection and Diagnosis, Fault-Tolerant Control, and Fault-Tolerant Guidance; 2.1.2 Interaction Between FDD, FTC, and FTG; 2.1.3 Chapter Organization; 2.2 Industrial State-of-Practice; 2.2.1 General Ideas; 2.2.2 Aeronautics; 2.2.3 Space Missions; 2.3 Review of Academic Advanced Results; 2.3.1 Introduction; 2.3.2 Analytical or Model-Based FDD; 2.3.3 Recovery Aspects: FTC and FTG
2.4 Toward Advanced Model-Based Techniques for Flight Vehicles2.4.1 Needs, Requirements, and Constraints; 2.4.2 Case Studies; 2.5 Conclusions; References; Chapter 3: Robust Detection of Oscillatory Failure Case in Aircraft Control Surface Servo-Loops; 3.1 Introduction and Motivations; 3.1.1 Primary Aircraft Control Surfaces; 3.1.2 The Link Between FDD of Control Surfaces and Aircraft Structural Design; 3.1.3 Oscillatory Failure Case; 3.2 OFC in Aircraft Control Surface Servo-Loop; 3.2.1 Description; 3.2.2 State-of-Practice: In-Service A380 Aircraft Example
184.108.40.206 Nonlinear Hydraulic Actuator Model220.127.116.11 Fault Detection; 18.104.22.168 A Flight Test Example; 3.2.3 Motivations for an Advanced Model-Based Approach; 3.3 Verification and Validation Tools; 3.3.1 Airbus Aircraft Benchmark (AAB); 3.3.2 Functional Engineering Simulator (FES); 3.3.3 Industrial Assessment Criteria; 22.214.171.124 Quantitative Assessment; 126.96.36.199 Qualitative Assessment; 3.4 Nonlinear Observer Design; 3.4.1 OFC Detectability; 3.4.2 Proposed Detection Algorithm; 188.8.131.52 Stability Analysis; 3.4.3 Decision-Making Rule; 3.4.4 Experimental Results
3.5 Fault Reconstruction via Sliding-Mode Differentiation3.5.1 Design of Hybrid Differential Observer; 184.108.40.206 Differentiator: Boundedness and Accuracy of Derivatives; 220.127.116.11 Fault Reconstruction; 3.5.2 Experimental Results; 18.104.22.168 Airbus Aircraft Benchmark Results; 22.214.171.124 FES Parametric Simulation Results; 126.96.36.199 Implementation Aspects; 3.6 Conclusion; References; Chapter 4: Robust Detection of Abnormal Aircraft Control Surface Position for Early System Reconfiguration; 4.1 Introduction; 4.2 Industrial State-of-Practice; 4.3 Need for Improvement; 4.4 A Dedicated Kalman-Based Solution
4.4.1 Runaway188.8.131.52 Fault Modeling; 184.108.40.206 Filter Design; 220.127.116.11 Optimization of the Filter Parameters; 4.4.2 Jamming; 4.5 Experimental Results; 4.5.1 Airbus Aircraft Benchmark (AAB) and Real Flight Data; 18.104.22.168 Runaway Case; 22.214.171.124 Performance and Robustness Evaluation; 126.96.36.199 Jamming Case; 4.5.2 Validation and Verification on Airbus Test Facilities; 188.8.131.52 Experimental Results Provided by the SIB; 184.108.40.206 Real Flight Tests; 4.6 Conclusion; References; Chapter 5: Failure Detection and Compensation for Aircraft Inertial System; 5.1 Introduction
5.2 Failure Detection and Isolation in Aircraft Inertial System
Fault Diagnosis and Fault-Tolerant Control and Guidance for Aerospace demonstrates the attractive potential of recent developments in control for resolving such issues as flight performance, self protection and extended-life structures. Importantly, the text deals with a number of practically significant considerations: tuning, complexity of design, real-time capability, evaluation of worst-case performance, robustness in harsh environments, and extensibility when development or adaptation is required. Coverage of such issues helps to draw the advanced concepts arising from academic research b
Description based upon print version of record.