Investigations for the synchronized operation of a hybrid actuator configuration in redundant flight control systems

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1. Verfasser: Cochoy, Olaf 1978- (VerfasserIn)
Format: Abschlussarbeit Buch
Sprache:English
Veröffentlicht: Aachen Shaker 2009
Schriftenreihe:Schriftenreihe Flugzeug-Systemtechnik 2009,5
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Datensatz im Suchindex

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adam_text 5.1.1 PERFORMANCE AND OPERATIONAL REQUIREMENTS 56 CONTENTS NOMENCLATURE IX 1 INTRODUCTION 1 1.1 MOTIVATION 4 1.2 STATE OF THE ART 5 1.2.1 FLY-BY-WIRE PRIMARY FLIGHT CONTROL ACTUATION SYSTEMS .... 5 1.2.2 ELECTRICALLY POWERED PRIMARY FLIGHT CONTROL ACTUATORS .... 7 1.2.3 ACTUATOR POSITION CONTROL LOOPS 11 1.3 OBJECTIVES, SCOPE AND STRUCTURE OF THE THESIS 12 2 HYBRID CONFIGURATION WITH ELECTRO-MECHANICAL AND ELECTRO-HYDRAULIC AC- TUATORS 15 2.1 DIFFERENCE OF THE ACTUATORS IN SETUP AND FUNCTION 15 2.2 INTEGRATION OF EMA IN PRIMARY FLIGHT CONTROLS 18 2.3 OPERATING MODES 20 2.4 QUALITATIVE COMPARISON OF ELECTRO-MECHANICAL ACTUATOR DESIGNS ... 21 3 TEST RIG 25 3.1 CONCEPT AND DESIGN 25 3.2 SCOPE OF EXPERIMENTS 28 4 MODELING OF THE HYBRID ACTUATOR CONFIGURATION 33 4.1 NONLINEAR MODELS 33 4.1.1 ELECTRO-HYDRAULIC SERVO-ACTUATOR 34 4.1.2 ELECTRO-MECHANICAL ACTUATOR 36 4.1.3 CONTROL SURFACE 41 4.1.4 COMBINED NONLINEAR MODEL OF THE HYBRID CONFIGURATION ... 41 4.2 LINEAR SYSTEM MODELS 43 4.2.1 LINEARIZATION AND COMBINATION OF MODELS 43 4.2.2 MODEL ORDER REDUCTION 48 4.3 EXPERIMENTAL MODEL VERIFICATION 50 5 CONTROL CONCEPTS FOR THE OPERATION OF THE HYBRID SYSTEM 55 5.1 REQUIREMENTS AND ASSUMPTIONS FOR CONTROLLER DESIGN 56 BIBLIOGRAFISCHE INFORMATIONEN HTTP://D-NB.INFO/999024698 DIGITALISIERT DURCH VIII CONTENTS 5.1.2 SYSTEM DEGRADATION 58 5.1.3 ACTUATOR LOAD SENSING 59 5.2 SINGLE LOOP CONTROL CONCEPT 63 5.2.1 DESIGN OF SINGLE CONTROL LOOPS 63 5.2.2 ACTUATOR DYNAMICS ADAPTATION AND ACTIVE/PASSIVE OPERATION . 64 5.2.3 SIGNAL FEEDBACK FOR FORCE FIGHT COMPENSATION IN ACTIVE/ACTIVE OPERATING MODE 67 5.2.4 ACTIVE/NO-LOAD OPERATING MODE 71 5.3 MULTIVARIABLE CONTROL CONCEPT 78 5.3.1 REQUIREMENTS AND ASSUMPTIONS 78 5.3.2 LOG CONTROLLER DESIGN 81 5.3.3 ROBUSTNESSOF THE MULTIVARIABLE CONTROLLERS 97 6 EXPERIMENTAL VERIFICATION AND COMPARISON OF CONTROL CONCEPTS 107 6.1 EXPERIMENTAL VERIFICATION 107 6.1.1 SINGLE-LOOP ACTIVE/ACTIVE VERIFICATION 108 6.1.2 SINGLE-LOOP ACTIVE/NO-LOAD VERIFICATION 110 6.1.3 MULTIVARIABLE ACTIVE/ACTIVE VERIFICATION 112 6.1.4 MULTI VARIABLE ACTIVE/NO-LOAD VERIFICATION 114 6.2 CONCEPT COMPARISON 116 7 FULL FLIGHT CONTROL SYSTEM DEMONSTRATION WITH HYBRID ACTUATION 123 8 CONCLUSIONS AND FUTURE WORK 129 BIBLIOGRAPHY 133 A MODEL PARAMETERS 139 * SIMULATION AND EXPERIMENTAL DATA 141
any_adam_object 1
author Cochoy, Olaf 1978-
author_GND (DE-588)140150447
author_facet Cochoy, Olaf 1978-
author_role aut
author_sort Cochoy, Olaf 1978-
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dewey-ones 629 - Other branches of engineering
dewey-raw 629.13236
dewey-search 629.13236
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discipline Maschinenbau / Maschinenwesen
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spelling Cochoy, Olaf 1978- Verfasser (DE-588)140150447 aut
Investigations for the synchronized operation of a hybrid actuator configuration in redundant flight control systems Olaf Cochoy
Aachen Shaker 2009
XIV, 144 S. graph. Darst.
txt rdacontent
n rdamedia
nc rdacarrier
Schriftenreihe Flugzeug-Systemtechnik 2009,5
Zugl.: Hamburg, Techn. Univ., Diss., 2009
Fly by wire (DE-588)4442360-3 gnd rswk-swf
Aktor (DE-588)4198914-4 gnd rswk-swf
Reglerentwurf (DE-588)4177447-4 gnd rswk-swf
Redundanz (DE-588)4157937-9 gnd rswk-swf
(DE-588)4113937-9 Hochschulschrift gnd-content
Fly by wire (DE-588)4442360-3 s
Aktor (DE-588)4198914-4 s
Redundanz (DE-588)4157937-9 s
Reglerentwurf (DE-588)4177447-4 s
DE-604
Schriftenreihe Flugzeug-Systemtechnik 2009,5 (DE-604)BV023084705 2009,5
DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=024573266&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis
spellingShingle Cochoy, Olaf 1978-
Investigations for the synchronized operation of a hybrid actuator configuration in redundant flight control systems
Schriftenreihe Flugzeug-Systemtechnik
Fly by wire (DE-588)4442360-3 gnd
Aktor (DE-588)4198914-4 gnd
Reglerentwurf (DE-588)4177447-4 gnd
Redundanz (DE-588)4157937-9 gnd
subject_GND (DE-588)4442360-3
(DE-588)4198914-4
(DE-588)4177447-4
(DE-588)4157937-9
(DE-588)4113937-9
title Investigations for the synchronized operation of a hybrid actuator configuration in redundant flight control systems
title_auth Investigations for the synchronized operation of a hybrid actuator configuration in redundant flight control systems
title_exact_search Investigations for the synchronized operation of a hybrid actuator configuration in redundant flight control systems
title_full Investigations for the synchronized operation of a hybrid actuator configuration in redundant flight control systems Olaf Cochoy
title_fullStr Investigations for the synchronized operation of a hybrid actuator configuration in redundant flight control systems Olaf Cochoy
title_full_unstemmed Investigations for the synchronized operation of a hybrid actuator configuration in redundant flight control systems Olaf Cochoy
title_short Investigations for the synchronized operation of a hybrid actuator configuration in redundant flight control systems
title_sort investigations for the synchronized operation of a hybrid actuator configuration in redundant flight control systems
topic Fly by wire (DE-588)4442360-3 gnd
Aktor (DE-588)4198914-4 gnd
Reglerentwurf (DE-588)4177447-4 gnd
Redundanz (DE-588)4157937-9 gnd
topic_facet Fly by wire
Aktor
Reglerentwurf
Redundanz
Hochschulschrift
url http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=024573266&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA
volume_link (DE-604)BV023084705
work_keys_str_mv AT cochoyolaf investigationsforthesynchronizedoperationofahybridactuatorconfigurationinredundantflightcontrolsystems