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Fault Diagnosis and Fault-Tolerant Control and Guidance for Aerospace Vehicles: From Theory to Application

Kataloginformation Katalogdatensatz500183669 .

Kataloginformation
Feldname	Details
Vorliegende Sprache	eng
Hinweise auf parallele Ausgaben	414530756 Druckausg.: ‡Fault diagnosis and fult-tolerant control and guidance for aerospace vehicles
ISBN	978-1-4471-5312-2
Name	Zolghadri, Ali
Name	Henry, David
Name ANZEIGE DER KETTE	Henry, David
Name	Cieslak, Jérôme
	Efimov, Denis
	Goupil, Philippe
T I T E L	Fault Diagnosis and Fault-Tolerant Control and Guidance for Aerospace Vehicles
Zusatz zum Titel	From Theory to Application
Verlagsort	London
Verlag	Springer London
Erscheinungsjahr	2014
Erscheinungsjahr	2014
Umfang	Online-Ressource (XVI, 216 p. 126 illus., 75 illus. in color, online resource)
Reihe	Advances in Industrial Control
Notiz / Fußnoten	Description based upon print version of record
Weiterer Inhalt	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. 3.2.2.1 Nonlinear Hydraulic Actuator Model3.2.2.2 Fault Detection; 3.2.2.3 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; 3.3.3.1 Quantitative Assessment; 3.3.3.2 Qualitative Assessment; 3.4 Nonlinear Observer Design; 3.4.1 OFC Detectability; 3.4.2 Proposed Detection Algorithm; 3.4.2.1 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; 3.5.1.1 Differentiator: Boundedness and Accuracy of Derivatives; 3.5.1.2 Fault Reconstruction; 3.5.2 Experimental Results; 3.5.2.1 Airbus Aircraft Benchmark Results; 3.5.2.2 FES Parametric Simulation Results; 3.5.2.3 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 Runaway4.4.1.1 Fault Modeling; 4.4.1.2 Filter Design; 4.4.1.3 Optimization of the Filter Parameters; 4.4.2 Jamming; 4.5 Experimental Results; 4.5.1 Airbus Aircraft Benchmark (AAB) and Real Flight Data; 4.5.1.1 Runaway Case; 4.5.1.2 Performance and Robustness Evaluation; 4.5.1.3 Jamming Case; 4.5.2 Validation and Verification on Airbus Test Facilities; 4.5.2.1 Experimental Results Provided by the SIB; 4.5.2.2 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
Titelhinweis	Druckausg.: ‡Fault diagnosis and fult-tolerant control and guidance for aerospace vehicles
ISBN	ISBN 978-1-4471-5313-9
Klassifikation	TJFM
	TEC004000
	629.8
	629.11
	TJ212-225
	ZQ 9940
Kurzbeschreibung	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
1. Schlagwortkette	Flugregelung
	Fehlererkennung
	Fehlertoleranz
SWB-Titel-Idn	395813867
Signatur	Springer E-Book
Bemerkungen	Elektronischer Volltext - Campuslizenz
Elektronische Adresse	$uhttp://dx.doi.org/10.1007/978-1-4471-5313-9
Internetseite / Link	Volltext
Siehe auch	Volltext
Siehe auch	Cover

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