Fault tolerant flight control: a benchmark challenge
Gespeichert in:
| Weitere Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Berlin ; Heidelberg
Springer
2010
|
| Schriftenreihe: | Lecture notes in control and information sciences
399 |
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | Literaturangaben |
| Beschreibung: | XXII, 586 S. Ill., graph. Darst. 24 cm |
| ISBN: | 9783642116896 |
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Datensatz im Suchindex
| _version_ | 1804143192029790208 |
|---|---|
| adam_text | 1.4 EARLIER ACCOMPLISHMENTS IN THIS FIELD, SOURCE: [40] 40 CONTENTS PART
I SURVIVING THE IMPROBABLE: TOWARDS RESILIENT AIRCRAFT CONTROL 1
INTRODUCTION 3 THOMAS LOMBAERTS, HAFID SMAILI, JAN BREEMAN 1.1 TOWARDS
MORE RESILIENT FLIGHT CONTROL 3 1.2 HISTORY OF FLIGHT CONTROL SYSTEMS,
SOURCE: [40] 4 1.2.1 MECHANICAL [33], [35] 6 1.2.2 HYDRO-MECHANICAL
[33], [35] 6 1.2.3 FLY-BY-WIRE RIGHT CONTROL [33], [35], [34] 7 1.2.4
FAULT TOLERANT CONTROL IN FLY-BY-WIRE SYSTEMS, SOURCES: [40] 10 1.2.5
AIRBUS PHILOSOPHY, SOURCES: [22], [30] 11 1.2.6 BOEING PHILOSOPHY,
SOURCES: [24], [42] 12 1.2.7 SHORT CASE STUDY OF OTHER FAULT TOLERANT
SYSTEMS, SOURCE: [24] 14 1.2.8 A FINAL NOTE ON FAULT TOLERANCE
PROPERTIES INCORPORATED IN CURRENT FLY BY WIRE FLIGHT CONTROL SYSTEMS 20
1.3 RATIONALE OF DAMAGE TOLERANT CONTROL - AIRCRAFT ACCIDENT SURVEY 21
1.3.1 AMERICAN AIRLINES FLIGHT AA191, SOURCE: [27] 22 1.3.2 JAPAN
AIRLINES FLIGHT JL123, SOURCE: [27] 26 1.3.3 UNITED AIRLINES FLIGHT
UA232, SOURCE: [27] 28 1.3.4 EL AL CARGO FLIGHT LY1862, SOURCE: [40] 30
1.3.5 USAIR FLIGHT 427 AND UNITED AIRLINES FLIGHT 585, SOURCES: [4],
[9], [5] 32 1.3.6 DHL CARGO FLIGHT ABOVE BAGHDAD, SOURCES: [31], [32] 36
1.3.7 FINAL NOTE ON ACCIDENT ANALYSIS 38 BIBLIOGRAFISCHE INFORMATIONEN
HTTP://D-NB.INFO/1000032779 DIGITALISIERT DURCH X CONTENTS 1.4.1
SELF-REPAIRING FLIGHT CONTROL SYSTEM (SRFCS) PROGRAM 40 1.4.2 MD-11
PROPULSION CONTROLLED AIRCRAFT (PCA) 41 1.4.3 NASA INTELLIGENT FLIGHT
CONTROL SYSTEM (IFCS) F-15 PROGRAM 41 1.5 RESEARCH CHALLENGES AND
OBJECTIVES 42 REFERENCES 43 2 FAULT TOLERANT FLIGHT CONTROL - A SURVEY
47 MICHEL VERHAEGEN, STOYAN KANEV, REDOUANE HALLOUZI, COLIN JONES, JAN
MACIEJOWSKI, HAFID SMAIL 2.1 WHY FAULT TOLERANT CONTROL? 47 2.2 FAULT
CLASSIFICATION 49 2.3 MODELLING FAULTS 51 2.3.1 MULTIPLICATIVE FAULTS 51
2.3.2 ADDITIVE FAULTS 53 2.3.3 COMPONENT FAULTS 54 2.4 MAIN COMPONENTS
IN AN FTC SYSTEM 55 2.5 FTC PROBLEM FORMULATION 58 2.5.1 PASSIVE FAULT
TOLERANT CONTROL 61 2.5.2 ACTIVE FAULT TOLERANT CONTROL 62 2.6
STATE-OF-THE-ART IN FAULT TOLERANT FLIGHT CONTROL 63 2.6.1
CLASSIFICATION OF RECONFIGURABLE CONTROL 63 2.6.2 MULTIPLE MODEL CONTROL
64 2.6.3 CONTROL ALLOCATION (CA) 69 2.6.4 ADAPTIVE FEEDBACK
LINEARIZATION VIA ARTIFICIAL NEURAL NETWORK 71 2.6.5 SLIDING MODE
CONTROL (SMC) 74 2.6.6 EIGENSTRUCTURE ASSIGNMENT (EA) 75 2.6.7 MODEL
REFERENCE ADAPTIVE CONTROL (MRAC) 78 2.6.8 MODEL PREDICTIVE CONTROL 80
2.6.9 MODEL FOLLOWING 81 2.6.10 ADAPTIVE CONTROL 82 2.7 COMPARISON OF
FAULT TOLERANT FLIGHT CONTROL METHODS 83 REFERENCES 85 3 CONTENTS XI
3.2.6 -BOO FAULT ESTIMATION APPROACH 104 3.2.7 NON-LINEAR FDD METHOD 107
3.2.8 SLIDING MODE OBSERVER 109 3.3 APPLICATION EXAMPLES 109 3.3.1
APPLICATION TO OSCILLATORY FAILURE CASE (OFC) 110 3.3.2 SIMULATED
AIRCRAFT MODEL FDD 110 3.3.3 AEROSPACE MISSION APPLICATION EXAMPLES 113
3.3.4 ROBUST DIAGNOSIS FOR MARS EXPRESS SATELLITE THRUSTER FAULTS 116
3.4 CONCLUSION 120 REFERENCES 121 4 REAL-TIME IDENTIFICATION OF AIRCRAFT
PHYSICAL MODELS FOR FAULT TOLERANT FLIGHT CONTROL 129 PING CHU, JAN
ALBERT (BOB) MULDER, JAN BREEMAN 4.1 INTRODUCTION 129 4.2 HISTORY OF
AIRCRAFT MODEL IDENTIFICATION AT DELFT UNIVERSITY OF TECHNOLOGY 130 4.3
THE TWO STEP METHOD 135 4.3.1 DECOMPOSITION OF AIRCRAFT STATE AND
PARAMETER ESTIMATION 136 4.3.2 ESTIMATION PROPERTIES 144 4.3.3
TECHNIQUES TO COPE WITH ESTIMATION BIASES 146 4.4 ON-LINE PARAMETER
ESTIMATION USING LEAST SQUARES AND TOTAL LEAST SQUARES METHODS 146 4.4.1
PRELIMINARIES 147 4.4.2 SEQUENTIAL TOTAL LEAST SQUARES (REF. [34]) 148
4.4.3 SUMMARY OF TLS METHOD 149 4.5 REAL-TIME IDENTIFICATION OF AIRCRAFT
PHYSICAL MODEL FOR FAULT TOLERANT FLIGHT CONTROL, [13] 149 4.6
CONCLUSIONS 152 REFERENCES 153 5 INDUSTRIAL PRACTICES IN FAULT TOLERANT
CONTROL 157 PHILIPPE GOUPIL 5.1 INTRODUCTION 157 5. XII CONTENTS PART II
RECOVER: THE BENCHMARK CHALLENGE 6 RECOVER: A BENCHMARK FOR INTEGRATED
FAULT TOLERANT FLIGHT CONTROL EVALUATION 171 HAFID SMAILI, JAN BREEMAN,
THOMAS LOMBAERTS, DIEDERICK JOOSTEN 6.1 INTRODUCTION 171 6.2 FLIGHT 1862
ACCIDENT RECONSTRUCTION AND SIMULATION 172 6.2.1 SEQUENCE OF EVENTS 173
6.2.2 ANALYSIS OF RIGHT 1862 176 6.2.3 FAILURE MODE CONFIGURATION 180
6.2.4 FLIGHT DATA RECONSTRUCTION AND SIMULATION 181 6.3 GARTEUR RECOVER
BENCHMARK 194 6.3.1 DESCRIPTION 194 6.3.2 IMPLEMENTATION 197 6.3.3 FAULT
SCENARIOS SPECIFICATION 200 6.3.4 GRAPHICAL USER INTERFACE 206 6.3.5
AIRCRAFT VISUALISATION 209 6.3.6 USER EXAMPLE 210 6.3.7 AIRCRAFT
CHARACTERISTICS 212 6.4 GARTEUR RECOVER BENCHMARK APPLICATIONS 218 6.5
CONCLUSION 219 REFERENCES 220 7 ASSESSMENT CRITERIA AS SPECIFICATIONS
FOR RECONFIGURING FLIGHT CONTROL 223 THOMAS LOMBAERTS, DIEDERICK
JOOSTEN, HAFID SMAILI, JAN BREEMAN 7.1 INTRODUCTION 223 7.2
SPECIFICATION MODELLING 224 7.2.1 GENERAL EVALUATION CRITERIA 225 7.2.2
TEST MANOEUVRES FOR QUALIFICATION 227 7.3 DISCUSSION 239 REFERENCES 243
PART III DESIGN METHODS AND BENCHMARK ANALYSIS 8 FAULT TOLERANT CONTROL
USING SLIDING MODES WITH ON-LINE CONTROL ALLOCATION 247 HALI CONTENTS
XIII 8.3 CONTROLLER DESIGN 254 8.3.1 FAULT TOLERANT CONTROLLER DESIGN
256 8.3.2 HEADING AND ALTITUDE CONTROL AND EPR CONTROL MIXING 260 8.3.3
ILS LANDING 261 8.3.4 FAULT TOLERANT CONTROL SIMULATION RESULTS 264 8.4
CONCLUSIONS 270 REFERENCES 270 9 AN ADAPTIVE FAULT-TOLERANT FCS FOR A
LARGE TRANSPORT AIRCRAFT ... 273 ADOLFO SOLLAZZO, GIANFRANCO MORANI,
ANDREA GIOVANNINI 9.1 FAULT-TOLERANT FCS 273 9.1.1 ADAPTIVE
MODEL-FOLLOWING 274 9.1.2 THE SCAS ARCHITECTURE 277 9.1.3 LIMITATIONS
AND PRACTICAL SOLUTIONS 279 9.2 THE CLASSIC A/P 280 9.3 NUMERICAL
VALIDATION 280 9.4 FUTURE DEVELOPMENT 287 9.5 CONCLUSIONS 289 REFERENCES
290 10 SUBSPACE PREDICTIVE CONTROL APPLIED TO FAULT-TOLERANT CONTROL
.... 293 REDOUANE HALLOUZI, MICHEL VERHAEGEN 10.1 INTRODUCTION 293 10.2
ARCHITECTURE OF THE FAULT-TOLERANT CONTROL SYSTEM 295 10.2.1 CONTROL
LOOPS 295 10.2.2 FAULT ISOLATION 296 10.3 CLOSED-LOOP SUBSPACE
PREDICTIVE CONTROL 297 10.3.1 CLOSED-LOOP SUBSPACE PREDICTOR (CLSP) 297
10.3.2 CLOSED-LOOP SUBSPACE PREDICTOR INTEGRATED WITH A PREDICTIVE
CONTROL LAW 301 10.4 SPC (RE-)CONFIGURATION 303 10.5 SIMULATION RESULTS
305 10.5.1 TRAJECTORY FOLLOWING FOR THE NOMINAL CASE 306 10.5.2
TRAJECTORY FOLLOWING FOR ELEVATOR LOCK-IN-PLACE 307 10.5.3 TRAJECTORY
FOLLOWING FOR RUDDER RUNAWAY 309 10.5. XIV CONTENTS 11 FAULT-TOLERANT
CONTROL THROUGH A SYNTHESIS OF MODEL-PREDICTIVE CONTROL AND NONLINEAR
INVERSION 319 D.A. JOOSTEN, T.J.J. VAN DEN BOOM, M. VERHAEGEN 11.1
INTRODUCTION 319 11.2 OVERALL CONTROL-SETUP 320 11.2.1 MODEL STRUCTURE
322 11.2.2 NONLINEAR DYNAMIC INVERSION 322 11.2.3 MODEL PREDICTIVE
CONTROL 324 11.2.4 CONTROL ALLOCATION 327 11.3 MODELING AND DYNAMIC
INVERSION OF THE BENCHMARK MODEL 327 11.4 SIMULATION RESULTS 331 11.4.1
REFERENCE TRACKING: STABILISER RUNAWAY 331 11.4.2 RIGHT TURN AND
LOCALISER INTERCEPT 332 11.5 CONCLUSION 335 REFERENCES 335 12 A FTC
STRATEGY FOR SAFE RECOVERY AGAINST TRIMMABLE HORIZONTAL STABILIZER
FAILURE WITH GUARANTEED NOMINAL PERFORMANCE 337 JEROME CIESLAK, DAVID
HENRY, ALI ZOLGHADRI 12.1 INTRODUCTION 337 12.2 NOMENCLATURE 339 12.3
PROBLEM STATEMENT 340 12.4 MODEL-BASED FDI SCHEMES: SOME ASSUMPTIONS FOR
AN INTEGRATED FDI/FTC DESIGN APPROACH 344 12.4.1 ANALYSIS OF THE FTC
LOOP 344 12.4.2 SOME OUTLINES FOR THE DESIGN 345 12.4.3 THE CASE OF AN
OBSERVER-BASED FDI SCHEME 346 12.5 IMPORTANT ISSUES ABOUT STABILITY AND
PERFORMANCE IN FAULTY SITUATIONS 346 12.6 FM-AG16 FTC PROBLEM 347 12.6.1
MODELLING THE AIRCRAFT DYNAMICS 347 12.6.2 MODELING THE AUTOFLIGHT AND
FCS SYSTEMS 350 12.6.3 DESIGN OF K(S) 35 CONTENTS XV 13.2 ON LINE
NONLINEAR DAMAGED AIRCRAFT MODEL IDENTIFICATION: TWO STEP METHOD 364
13.2.1 AIRCRAFT STATE ESTIMATION 366 13.2.2 AERODYNAMIC MODEL
IDENTIFICATION 368 13.3 REAL TIME AERODYNAMIC MODEL IDENTIFICATION 371
13.4 APPLICATION ON THE BOEING 747 SIMULATOR 372 13.4.1 TRIM HORIZONTAL
STABILIZER (THS) RUNAWAY 373 13.4.2 LOSS OF THE VERTICAL TAIL 373 13.4.3
FEEDBACK OF AIRCRAFT STABILITY AND CONTROL EFFECTOR INFORMATION TO THE
PILOT 375 13.5 TRIGGER FOR RECONFIGURATION 376 13.6 RECONFIGURING
CONTROL: ADAPTIVE NONLINEAR DYNAMIC INVERSION 377 13.6.1 AUTOPILOT
CONTROL: ASSESSMENT CRITERIA 382 13.7 COMPUTATIONAL LOAD 395 13.8
CONCLUSIONS 395 13.9 CURRENT AND FUTURE WORK 396 REFERENCES 396 14 A
COMBINED FAULT DETECTION, IDENTIFICATION AND RECONFIGURATION SYSTEM
BASED AROUND OPTIMAL CONTROL ALLOCATION 399 NICHOLAS SWAIN, SHADHANAN
MANICKAVASAGAR 14.1 BACKGROUND 399 14.1.1 CONTROL ALLOCATION 399 14.1.2
FAULT DETECTION AND IDENTIFICATION 402 14.1.3 SOFTWARE AND HARDWARE
TESTING 403 14.2 INTRODUCTION 403 14.3 FAULT TOLERANT CONTROL SYSTEM
OVERVIEW 405 14.3.1 SENSORS 405 14.3.2 OUTER-LOOP CONTROLLER/AUTOPILOT
406 14.3.3 NON-LINEAR DYNAMIC INVERSION 406 14.3.4 DIRECT CONTROL
ALLOCATION 407 14.3.5 AERODYNAMIC FDI 411 14.3.6 ACTUATOR FDI 414 14.3.7
FLIGHT ENVELOPE PROTECTION 416 14. XVI CONTENTS 15 DETECTION AND
ISOLATION OF ACTUATOR/SURFACE FAULTS FOR A LARGE TRANSPORT AIRCRAFT 423
ANDRAS VARGA 15.1 INTRODUCTION 423 15.2 DESIGN OF LEAST ORDER SCALAR
OUTPUT DETECTORS 424 15.3 SOLVING FAULT ISOLATION PROBLEMS 426 15.4
COMPUTATIONAL ASPECTS 429 15.5 MONITORING ACTUATOR FAILURES 430 15.5.1
COMPONENT LEVEL MONITORING 431 15.5.2 SYSTEM LEVEL MONITORING 433 15.5.3
PITCH AXIS FAULT MONITORING 435 15.5.4 GEAR AND ROLL AXES FAULT
MONITORING 439 15.6 SUMMARY OF ACHIEVED RESULTS AND NEEDS FOR FURTHER
ANALYSIS 441 REFERENCES 442 PART IV REAL-TIME FLIGHT SIMULATOR
ASSESSMENT 16 REAL-TIME ASSESSMENT AND PILOTED EVALUATION OF FAULT
TOLERANT FLIGHT CONTROL DESIGNS IN THE SIMONA RESEARCH FLIGHT SIMULATOR
451 OLAF STROOSMA, THOMAS LOMBAERTS, HAFID SMAILI, MARK MULDER 16.1
INTRODUCTION 451 16.2 EVALUATION METHOD 453 16.2.1 EXPERIMENT DESIGN 453
16.2.2 DEPENDENT MEASURES 455 16.2.3 PARTICIPANTS 457 16.2.4 SIMULATOR
CONFIGURATION 457 16.2.5 PROCEDURE 463 16.3 RESULTS 468 16.4 CONCLUSIONS
471 APPENDIX 1 : FAILURE MODE TEST MATRIX 472 APPENDIX 2: COOPER HARPER
HANDLING QUALITIES RATING SCALE 474 REFERENCES 475 17 PILOTED EVALUATION
RESULTS OF A NONLINEAR DYNAMIC INVERSION BASED CONTROLLER USING ONLINE
PHYSICAL MODEL IDENTIFICATION 47 CONTENTS XVII 17.4.2 HANDLING QUALITIES
ANALYSIS RESULTS: CH RATINGS 486 17.4.3 PILOT WORKLOAD ANALYSIS RESULTS
491 17.5 CONCLUSIONS 498 REFERENCES 499 18 MODEL REFERENCE SLIDING MODE
FTC WITH SIMONA SIMULATOR EVALUATION: EL AL FLIGHT 1862 BIJLMERMEER
INCIDENT SCENARIO .... 501 HALIM ALWI, CHRISTOPHER EDWARDS, OLAF
STROOSMA, JAN ALBERT (BOB) MULDER 18.1 INTRODUCTION 501 18.2 A MODEL
REFERENCE SLIDING MODE CONTROL ALLOCATION SCHEME 502 18.3 CONTROLLER
DESIGN 506 18.3.1 LATERAL CONTROLLER DESIGN 507 18.3.2 LONGITUDINAL
CONTROLLER DESIGN 508 18.4 SIMONA IMPLEMENTATION 510 18.5 SIMONA FLIGHT
SIMULATOR RESULTS WITH EXPERIENCED PILOTS 510 18.5.1 SMC CONTROLLER
EVALUATION 511 18.6 CONCLUSIONS 517 REFERENCES 517 PARTV CONCLUSIONS 19
INDUSTRIAL REVIEW 521 PHILIPPE GOUPIL, ANDRES MARCOS 19.1 INTRODUCTION
521 19.2 CONSIDERATIONS FOR COMMERCIAL AIRCRAFT - AIRBUS 522 19.2.1
INDUSTRIAL LIMITATIONS AND CONSTRAINTS 523 19.2.2 AN AIRCRAFT
MANUFACTURER PERSPECTIVE 524 19.2.3 CONCLUSION 528 19.3 PERSPECTIVES FOR
AEROSPACE APPLICATIONS - DEIMOS SPACE 528 19.3.1 CONTEXT AND
SIGNIFICANCE OF THE FM-AG16 FOR SPACE SYSTEMS 530 19.3.2 ASSESSMENT OF
THE TECHNIQUES AND RESULTS 532 19.3.3 CONCLUSION 535 REFERENCES 535 20
CONCLUDING REMARKS 53
|
| any_adam_object | 1 |
| author2 | Edwards, Christopher 1966- |
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| author_GND | (DE-588)136868169 |
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| building | Verbundindex |
| bvnumber | BV036593755 |
| classification_rvk | SI 845 ZO 7276 |
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| dewey-raw | 629.13236 |
| dewey-search | 629.13236 |
| dewey-sort | 3629.13236 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Maschinenbau / Maschinenwesen Mathematik Verkehr / Transport |
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| id | DE-604.BV036593755 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T22:43:45Z |
| institution | BVB |
| isbn | 9783642116896 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-020514411 |
| oclc_num | 699869529 |
| open_access_boolean | |
| owner | DE-83 DE-573 |
| owner_facet | DE-83 DE-573 |
| physical | XXII, 586 S. Ill., graph. Darst. 24 cm |
| publishDate | 2010 |
| publishDateSearch | 2010 |
| publishDateSort | 2010 |
| publisher | Springer |
| record_format | marc |
| series | Lecture notes in control and information sciences |
| series2 | Lecture notes in control and information sciences |
| spelling | Fault tolerant flight control a benchmark challenge Christopher Edwards ... (eds.) Berlin ; Heidelberg Springer 2010 XXII, 586 S. Ill., graph. Darst. 24 cm txt rdacontent n rdamedia nc rdacarrier Lecture notes in control and information sciences 399 Literaturangaben Fly by wire (DE-588)4442360-3 gnd rswk-swf Fehlertoleranz (DE-588)4123192-2 gnd rswk-swf Fly by wire (DE-588)4442360-3 s Fehlertoleranz (DE-588)4123192-2 s DE-604 Edwards, Christopher 1966- (DE-588)136868169 edt Lecture notes in control and information sciences 399 (DE-604)BV005848579 399 DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=020514411&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Fault tolerant flight control a benchmark challenge Lecture notes in control and information sciences Fly by wire (DE-588)4442360-3 gnd Fehlertoleranz (DE-588)4123192-2 gnd |
| subject_GND | (DE-588)4442360-3 (DE-588)4123192-2 |
| title | Fault tolerant flight control a benchmark challenge |
| title_auth | Fault tolerant flight control a benchmark challenge |
| title_exact_search | Fault tolerant flight control a benchmark challenge |
| title_full | Fault tolerant flight control a benchmark challenge Christopher Edwards ... (eds.) |
| title_fullStr | Fault tolerant flight control a benchmark challenge Christopher Edwards ... (eds.) |
| title_full_unstemmed | Fault tolerant flight control a benchmark challenge Christopher Edwards ... (eds.) |
| title_short | Fault tolerant flight control |
| title_sort | fault tolerant flight control a benchmark challenge |
| title_sub | a benchmark challenge |
| topic | Fly by wire (DE-588)4442360-3 gnd Fehlertoleranz (DE-588)4123192-2 gnd |
| topic_facet | Fly by wire Fehlertoleranz |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=020514411&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| volume_link | (DE-604)BV005848579 |
| work_keys_str_mv | AT edwardschristopher faulttolerantflightcontrolabenchmarkchallenge |