Fault diagnosis and reconfiguration in flight control systems:
Gespeichert in:
Hauptverfasser: | , |
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Format: | Buch |
Sprache: | English |
Veröffentlicht: |
Boston <<[u.a.]>>
Kluwer Academic Publ.
2003
|
Schriftenreihe: | Cooperative systems
2 |
Online-Zugang: | Inhaltsverzeichnis |
Beschreibung: | XXVI, 342 S. Ill., graph. Darst. |
ISBN: | 1402076053 |
Internformat
MARC
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245 | 1 | 0 | |a Fault diagnosis and reconfiguration in flight control systems |c by Chingiz Hajiyev and Fikret Caliskan |
264 | 1 | |a Boston <<[u.a.]>> |b Kluwer Academic Publ. |c 2003 | |
300 | |a XXVI, 342 S. |b Ill., graph. Darst. | ||
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Datensatz im Suchindex
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adam_text | FAULT DIAGNOSIS AND RECONFIGURATION IN FLIGHT CONTROL SYSTEMS BY CHINGIZ
HAJIYEV ISTANBUL TECHNICAL UNIVERSITY, TURKEY AND FIKRET CALISKAN
ISTANBUL TECHNICAL UNIVERSITY, TURKEY KLUWER ACADEMIC PUBLISHERS
BOSTON/DORDRECHT/LONDON CONTENTS LIST OF FIGURES XIII LIST OF TABLES XIX
PREFACE XXI 1. INTRODUCTION 1 1.1. INTRODUCTION 1 1.2. FAULT DETECTION
AND ISOLATION 3 1.3. REDUNDANCY 5 1.4. PERFORMANCE OF FDI 7 1.5.
ROBUSTNESS 7 1.6. RECONFIGURATION AND FAULT TOLERANT FLIGHT CONTROL
SYSTEMS 9 1.6.1. SELF-REPAIRING FLIGHT CONTROL SYSTEMS 9 1.6.2. FAULT
DETECTION AND DYNAMIC RECONFIGURATION 10 1.6.3. ANALYTICAL REDUNDANCY 11
1.6.4. GAME THEORY AND REAL-TIME PARAMETER INSENSITIVE DISTURBANCE
ATTENUATING REDESIGN 12 1.6.5. TECHNIQUES FOR RECONFIGURATION 12 1.7.
SENSOR/ACTUATOR FAULT DIAGNOSIS 17 1.7.1. SENSOR FAULT DETECTION IN
FLIGHT CONTROL SYSTEMS 17 1.7.2. INTEGRATED SENSOR/ACTUATOR FDI AND
RECONFIGURABLE CONTROL FOR FAULT-TOLERANT FLIGHT CONTROL SYSTEM DESIGN
20 REFERENCES 21 2. GENERAL THEORY OF OBSERVERS 25 2.1. INTRODUCTION 25
2.2. THEORY AND DESIGN OF OBSERVERS 26 2.2.1. APPROACHES TO OBSERVER
DESIGN 29 2.3. PARAMETER INSENSITIVE OBSERVERS 36 2.4. ROBUSTNESS OF
OBSERVER-BASED CONTROLLERS 39 VLLL 2.4.1. AN OBSERVER ADJUSTMENT
PROCEDURE 42 2.5. ROBUST OBSERVERS: DOYLE-STEIN OBSERVER 45 2.6. FAILURE
INSENSITIVE LUENBERGER OBSERVER 51 2.7. CONCLUSION 54 REFERENCES 54 3.
LINEAR KALMAN FILTERING 55 3.1. INTRODUCTION 5 5 3.2. THE OPTIMUM LINEAR
DISCRETE KALMAN F : !TER 56 3.3. OPTIMUM DISCRETE KALMAN FILTER
STABILITY 61 3.4. DISCRETE KALMAN FILTER - CORRELATED SYSTEM AND
MEASUREMENT NOISE 62 3.5. GENERAL DISCRETE KALMAN FILTERING 65 3.6
DIVERGENCE IN THE KALMAN FILLER. SUBOPTIMAL KALMAN FILTERS 69 3.7 THE
METHODS OF NUMERICAL STABILIZATION OF KALMAN FILTERS. SQUARE ROOT
FILTERING 71 3.8. DIAGNOSTICS OF KALMAN FILTERING ALGORITHMS 72 3.8.1.
MONITORING CONDITIONS FOR THE SCALAR FILTER 73 3.8.2. DIAGNOSTICS OF THE
SQUARE ROOT FILTER 75 3.9. SUMMARY 83 REFERENCES 84 4. NONLINEAR
ESTIMATION AND SYSTEM IDENTIFICATION 87 4.1. INTRODUCTION 87 4.2.
LINEARIZED KALMAN FILTER 88 4.3. THE EXTENDED KALMAN FILTER 91 4.4.
DERIVATION OF EKF EQUATIONS FOR NONLINEAR FLIGHT DYNAMICS 92 4.4.1.
DERIVATION OF THE MATHEMATICAL MODEL OF THE AIRCRAFT LONGITUDINAL MOTION
93 4.4.2. DESIGN OF EKF TO ESTIMATE THE AIRCRAFT LONGITUDINAL MOTION 95
4.5. EKF AND SYSTEM IDENTIFICATION 103 4.5.1 AN EXAMPLE OF PARAMETER
IDENTIFICATION 104 4.6. STOPPING RULES FORMATION AND FAULTS DETECTION IN
PARAMETRIC IDENTIFICATION PROBLEMS 107 4.6.1. GENERATION OF STOPPING
RULES 109 4.6.2. FAULT DETECTION IN THE KALMAN FILTER 110 4.6.3.
COMPUTATION OF THE COVARIANCE MATRIX OF THE DISCREPANCY BETWEEN TWO
SUCCESSIVE ESTIMATES 112 4.7. AN EXPERIMENTAL EXAMPLE OF PARAMETER
IDENTIFICATION 114 4.8. CONCLUSION AND DISCUSSION 119 REFERENCES 120 IX
5. INTRODUCTION TO MONITORS, DETECTORS, AND DIAGNOSTICANS 123 5.-1.
INTRODUCTION 123 5.1.1 MODEL-FREE METHODS 124 5.1.2 MODEL-BASED FAULT
DIAGNOSIS 125 5.2. MONITORS 128 5.2.1 THE PARITY SPACE APPROACH 128
5.2.2 PARAMETER IDENTIFICATION APPROACH 130 5.2.3 DEDICATED OBSERVER
APPROACH 132 5.3. DETECTORS 136 5.3.1 HYPOTHESIS TESTING 137 5.3.2
NEYMANN-PEARSON CRITERION 142 5.4. DIAGNOSTICIANS 146 5.5. SUMMARY 151
REFERENCES 151 6. AN OVERVIEW OF ALGORITHMS FOR FAILURE DETECTION AND
ISOLATION 153 6.1. INTRODUCTION 6.2. FAILURE DETECTION TECHNIQUES 161
6.2.1 SENSOR LEVEL FAILURES 161 6.2.2 FAILURES IN COMPUTING SUBSYSTEM
AND LANES 170 6.2.3 ACTUATOR AND CONTROL SURFACE LEVEL FAILURES 171
6.2.4 ROBUSTNESS OF FAILURE DETECTION PROCESS TO PARAMETER CHANGES IN
DYNAMIC SYSTEMS 181 6.3. SUMMARY 183 REFERENCES 183 7. THE INNOVATION
APPROACH TO FAULT DETECTION 187 7.1. INTRODUCTION 187 7.2. THE
INNOVATION SEQUENCE 189 7.3. THE METHODS FOR CHECKING THE STATISTICAL
CHARACTERISTICS OF INNOVATION SEQUENCE 192 7.3.1. THE APPROPRIATENESS
CRITERIONS OF INNOVATION SEQUENCE TO THE WHITE NOISE 192 7.3.2. THE
CRITERIONS, CHECKING THE MEAN OF THE INNOVATION SEQUENCE 195 7.3.3. THE
CLASSICAL CRITERIONS, CHECKING THE COVARIANCE MATRICES OF THE INNOVATION
SEQUENCE 197 7.4. SOME NEW METHODS FOR CHECKING THE COVARIANCE MATRICES
OF INNOVATION SEQUENCE 204 7.4.1. CHECKING THE COVARIANCE MATRICES OF
THE INNOVATION SEQUENCE VIA THE STATISTICS OF RELATION BETWEEN TWO
QUADRATIC FORMS 204 7.4.2. CHECK OF THE GENERALIZED VARIANCE OF THE
NORMALIZED INNOVATION SEQUENCE 208 7.4.3. SIMULTANEOUS CHECKING THE MEAN
AND COVARIANCE MATRICES OF THE INNOVATION SEQUENCE 211 7.5. CONCLUSION
AND DISCUSSION 220 REFERENCES 221 8. SENSOR FAULT DETECTION AND
ISOLATION IN FLIGHT CONTROL SYSTEMS BASED ON INNOVATION APPROACH 225
8.1. INTRODUCTION 225 8.2. INNOVATION SEQUENCE APPLICATION TO AIRCRAFT
SENSOR FAULT DETECTION 226 8.2.1. SIMULATION OF AIRCRAFT DYNAMICS VIA
KALMAN FILTER 227 8.2.2. FAULT DETECTION BY VERIFYING THE INNOVATION
MEAN 228 8.2.3. FAULT DETECTION BY VERIFYING THE INNOVATION COVARIANCE
230 8.3. COMPARISON OF CHECKING COVARIANCE MATRIX ALGORITHMS 232 8.4.
FAULT DETECTION VIA SPECTRAL NORM OF INNOVATION MATRIX 243 8.5. SENSOR
FAULT ISOLATION ALGORITHM 248 8.6. AIRCRAFT APPLICATION OF SENSOR FAULT
ISOLATION ALGORITHM 252 8.7. CONCLUSION AND DISCUSSION 254 REFERENCES
255 9. ROBUST KALMAN FILTERS FOR FDI 259 9.1. INTRODUCTION 259 9.2.
ROBUST KALMAN FILTER INSENSITIVE TO ACTUATOR FAILURES 260 9.2.1
SIMULATION OF RKF BASED ON DOYLE-STEIN CONDITION 262 9.3. ROBUST KALMAN
FILTER INSENSITIVE TO ABNORMAL MEASUREMENTS 265 9.4. ROBUST KALMAN
FILTER INSENSITIVE TO SENSOR FAILURES 269 9.5. ACTUATOR FAULT DIAGNOSIS
BASED ON ROBUST KALMAN FILTER 271 9.5.1. KALMAN FILTER FOR ACTUATOR
PARAMETER ESTIMATION 271 9.5.2. ACTUATOR FAULT DETECTION ALGORITHM 273
9.5.3. AN ILLUSTRATIVE EXAMPLE 274 9.6. CONCLUSION AND DISCUSSION 280
REFERENCES 281 10. FLIGHT CONTROL RECONFIGURATION 283 10.1. INTRODUCTION
283 10.2 AN AUTOMATIC REDESIGN APPROACH FOR RESTRUCTURABLE CONTROL
SYSTEMS 284 10.2.1 INTRODUCTION 284 10.2.2. THE AUTOMATIC REDESIGN
PROCEDURE 285 10.2.3 DEVELOPMENT OF THE AUTOMATIC REDESIGN PROCEDURE 288
10.2.4. SOLUTION OF THE OPTIMIZATION PROBLEM 291 CH. HAJIYEV AND F.
CALISKAN XI 10.3. CONTROL SYSTEMS INSENSITIVITY TO VARIATIONS IN DYNAMIC
SYSTEM PARAMETERS 294 - 10.4. RECONFIGURATION BASED ON MIN-MAX TYPE
CRITERIA 296 10.4.1. THE MIN-MAX PRINCIPLE 296 10.4.2. PARAMETER
INSENSITIVE, DISTURBANCE ATTENUATING REDESIGN 297 10.4.3. SIMULATION OF
THE RECONFIGURATION ALGORITHM 301 10.5. THE EKF BASED RECONFIGURABLE
CONTROL 309 10.5.1. IDENTIFICATION OF THE CONTROL DISTRIBUTION MATRIX
309 10.5.2. THE EKF BASED RECONFIGURABLE CONTROL ALGORITHM 315 10.6.
FAULT-TOLERANT FLIGHT CONTROL SYSTEM BASED ON INNOVATION APPROACH 321
10.7. CONCLUSION AND DISCUSSION 324 REFERENCES 324 INDEX 327 ABOUT THE
AUTHORS 341
|
any_adam_object | 1 |
author | Hajiyev, Chingiz Caliskan, Fikret |
author_facet | Hajiyev, Chingiz Caliskan, Fikret |
author_role | aut aut |
author_sort | Hajiyev, Chingiz |
author_variant | c h ch f c fc |
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bvnumber | BV024510270 |
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ctrlnum | (OCoLC)248887270 (DE-599)BVBBV024510270 |
dewey-full | 629.135 |
dewey-hundreds | 600 - Technology (Applied sciences) |
dewey-ones | 629 - Other branches of engineering |
dewey-raw | 629.135 |
dewey-search | 629.135 |
dewey-sort | 3629.135 |
dewey-tens | 620 - Engineering and allied operations |
discipline | Verkehr / Transport |
format | Book |
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indexdate | 2024-07-09T22:01:06Z |
institution | BVB |
isbn | 1402076053 |
language | English |
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physical | XXVI, 342 S. Ill., graph. Darst. |
publishDate | 2003 |
publishDateSearch | 2003 |
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publisher | Kluwer Academic Publ. |
record_format | marc |
series | Cooperative systems |
series2 | Cooperative systems |
spelling | Hajiyev, Chingiz Verfasser aut Fault diagnosis and reconfiguration in flight control systems by Chingiz Hajiyev and Fikret Caliskan Boston <<[u.a.]>> Kluwer Academic Publ. 2003 XXVI, 342 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier Cooperative systems 2 Caliskan, Fikret Verfasser aut Cooperative systems 2 (DE-604)BV017968514 2 GBV Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=018484568&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
spellingShingle | Hajiyev, Chingiz Caliskan, Fikret Fault diagnosis and reconfiguration in flight control systems Cooperative systems |
title | Fault diagnosis and reconfiguration in flight control systems |
title_auth | Fault diagnosis and reconfiguration in flight control systems |
title_exact_search | Fault diagnosis and reconfiguration in flight control systems |
title_full | Fault diagnosis and reconfiguration in flight control systems by Chingiz Hajiyev and Fikret Caliskan |
title_fullStr | Fault diagnosis and reconfiguration in flight control systems by Chingiz Hajiyev and Fikret Caliskan |
title_full_unstemmed | Fault diagnosis and reconfiguration in flight control systems by Chingiz Hajiyev and Fikret Caliskan |
title_short | Fault diagnosis and reconfiguration in flight control systems |
title_sort | fault diagnosis and reconfiguration in flight control systems |
url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=018484568&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
volume_link | (DE-604)BV017968514 |
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