
Preliminary Programme - Session List
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Attention: Be advised that there might be changes till the congress, so please do not adjust your travel plans based on this preliminary programme.
Monday, 05. Sep 2022
07:00 - 08:00 | Registration |
08:00 - 09:00 | Opening Ceremony |
0.1 | ICAS Daniel & Florence Guggenheim Memorial Lecture, “Aeronautical Innovation – Swedish and European Perspectives”, Anders Blom, Sweden Chair: J.L. Azevedo ICAS President | |||
05. Sep 22 | 09:00 | 10:00 |
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10:00 - 10:30 | Coffee Break |
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05. Sep 22 | 10:30 | 11:00 | 1.1.1 |
THE SWEDISH AIR FORCE INTO THE FUTURE – AIMING FOR A HIGHER GROUND AND A SHARPER EDGE T. Petersson, Sweden | |||
05. Sep 22 | 11:00 | 11:30 | 1.1.2 |
BAE SYSTEMS ICAS BRIEF FUTURE COMBAT AIRCRAFT SYSTEM (FCAS) - THE COMPLEXITY OF THE SKILLS EQUATION Steve Hopkins, BAE Systems, United Kingdom; Ian Noakes, BAe Systems, United Kingdom | |||
05. Sep 22 | 11:30 | 12:00 | 1.1.3 |
FUTURE COMBAT AIR SYSTEMS: REQUIREMENTS AND TECHNOLOGIES G. M. Girard, Dassault Aviation, France | |||
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05. Sep 22 | 10:30 | 11:00 | 2.1.1 |
LARGE-SCALE MULTIFIDELITY AEROSTRUCTURAL OPTIMIZATION OF A TRANSPORT AIRCRAFT N. Y. Wu¹, C. A. Mader¹, J. R. R. A. Martins¹; ¹University of Michigan, United States Presenter: Neil Wu, University of Michigan | |||
05. Sep 22 | 11:00 | 11:30 | 2.1.2 |
REGIONAL JET RETROFITTING DESIGN: FROM STAKEHOLDERS’ NEEDS AND SYSTEM’S REQUIREMENTS TO MDAO WORKFLOW FORMULATION M. Mandorino¹, P. Della Vecchia¹, F. Nicolosi¹, S. Corcione¹, V. Trifari¹, G. Cerino, Leonardo Aircraft Division, Italy; M. Fioriti², C. Cabailero², T. Lefebvre, ONERA/DTIS, Université de Toulouse, France; ¹University of Naples Federico II, Italy ;²Politecnico di Torino, Italy | |||
05. Sep 22 | 11:30 | 12:00 | 2.1.3 |
COAST - A SIMULATION AND CONTROL FRAMEWORK TO SUPPORT MULTIDISCIPLINARY OPTIMIZATION AND AIRCRAFT DESIGN WITH CPACS D. Kiehn¹, J. Autenrieb¹, N. Fezans¹; ¹German Aerospace Center (DLR), Germany | |||
Reserve Paper | 2.1.R |
CERTIFICATION DRIVEN DESIGN FROM STAKEHOLDERS’ NEEDS TO MDAO FORMULATION WITHIN AGILE 4.0 PROJECT M Fioriti, Politecnico di Torino, Italy; C Cabaleiro, DLR, Germany; T Lefebvre, ONERA, France; P Della Vecchia¹, M Mandorino¹, S Liscouët-Hanke², A Jeyarai²; ¹Università di Napoli Federico II, Italy ;²Concordia University, Canada | |||||
Reserve Paper | 2.1.R |
OBJECT ORIENTED MULTI FIDELITY AIRCRAFT DESIGN TOOL FOR FIXED WING EVTOL UAVS T Seren, Chair of Aircraft Design - Technical University of Munich, Germany | |||||
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05. Sep 22 | 10:30 | 11:00 | 3.1.1 |
HIGH-SPEED COMPOUND HELICOPTER RESEARCH AT JAXA M. Sugiura¹, Y. Tanabe¹, N. Kobiki¹, H. Sugawara¹, K. Kimura¹; ¹JAXA, Japan | |||
05. Sep 22 | 11:00 | 11:30 | 3.1.2 |
DESIGN OF A FLYING V SUBSONIC TRANSPORT J. Benad¹, R. Vos¹; ¹Delft University of Technology, Netherlands | |||
05. Sep 22 | 11:30 | 12:00 | 3.1.3 |
DESIGN AND WIND TUNNEL TESTING OF A GENERAL AVIATION BLENDED WING BODY AIRCRAFT F Staub¹, T Tsuchiya¹; ¹The University of Tokyo, Japan | |||
Reserve Paper | 3.1.R |
DEVELOPMENT OF AN AERODYNAMIC ANALYSIS TOOL FOR BOUNDARY LAYER INGESTION CONCEPT DESIGN Xin Zhao¹, Carlos Xisto¹, Shia-Hui Peng, Chalmers University of Technology/FOI, Sweden; ¹Chalmers University of Technology, Sweden | |||||
Reserve Paper | 3.1.R |
EXPERIMENTAL ASSESSMENT OF A NEXT-GENERATION AIRLINER WITH BOUNDARY LAYER INGESTION P. D. Bravo-Mosquera¹, J. P. Eguea¹, H. D. Cerón-Muñoz¹, F. Catalano¹; ¹University of São Paulo, Brazil | |||||
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05. Sep 22 | 10:30 | 11:00 | 4.1.1 |
UNSTEADY TURBULENT FLOW SIMULATION OF ROTOR BLADES ON MOVING CARTESIAN GRIDS USING RECURSIVE FITTING APPROACH Keisuke Sugaya¹, Taro Imamura¹; ¹The University of Tokyo, Japan Presenter: Keisuke Sugaya, The University of Tokyo | |||
05. Sep 22 | 11:00 | 11:30 | 4.1.2 |
COMPUTATIONAL ANALYSIS OF SUPERSONIC FLOW AROUND A WEDGE AND A CYLINDER USING BUILDING-CUBE METHOD Kumpei Abe¹, Sayaka Miyazaki¹, Daisuke Sasaki¹, Shun Takahashi², Gohji Yamada²; ¹Kanazawa Institute of Technology, Japan ;²Tokai University, Japan | |||
05. Sep 22 | 11:30 | 12:00 | 4.1.3 |
ON THE INFLUENCE OF GRADIENT RECONSTRUCTION PROCEDURES OVER THE ACCURACY OF FINITE VOLUME BASED SCHEMES F. B. Oliveira, Instituto Tecnológico de Aeronáutica, Brazil; J. L. F. Azevedo, Instituto de Aeronáutica e Espaço, Brazil | |||
Reserve Paper | 4.1.R |
INVESTIGATION OF TWO-DIMENSIONAL VORTEX DYNAMICS IN V103 CASCADE CHANNEL Yihan Zhao¹, Yang Liu¹, Shuaichen Zhu¹, Hongyi Xu¹, Duo Wang¹; ¹Department of Aeronautics and Astronautics, Fudan University, China | |||||
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05. Sep 22 | 10:30 | 11:00 | 5.1.1 |
GARTEUR: NEARLY HALF A CENTURY OF EUROPEAN COLLABORATION IN AERONAUTICS RESEARCH P. Renzoni, Centro Italiano Ricerche Aerospaziali, Italy | |||
05. Sep 22 | 11:00 | 11:30 | 5.1.2 |
THE GROUP OF RESPONSABLES AERODYNAMICS GOR AD AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES P. Coustols, ONERA, France; F. Monge, INTA, Spain; 4 van der Ven, NLR, Netherlands; K. Richter, DLR, Germany; M. Tormalm, FOI, Sweden; L.R. Calavera, AIRBUS, Spain; B. Stefes, AIRUBS, Germany; D. Pagan, MBDA, France; P. Eliasson, SAAB, Sweden; M. Mallet, DASSAULT, France; R. Gemma, LEONARDO, Italy | |||
05. Sep 22 | 11:30 | 12:00 | 5.1.3 |
THE GARTEUR GROUP OF RESPONSABLES “STRUCTURES AND MATERIALS: AN OVERVIEW OF ACTIVITIES AND SUCCES STORIES B. Thuis, NLR, Netherlands | |||
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05. Sep 22 | 10:30 | 11:00 | 6.1.1 |
EXPERIMENTAL INVESTIGATION OF THE EFFECT OF THE YAW ANGLE ON THE DRAG REDUCTION RATE FOR TRAPEZOIDAL RIBLETS A INASAWA¹, R TANIGUCHI¹, M ASAI¹, M SASAMORI², M KURITA²; ¹Tokyo Metropolitan University, Japan ;²JAXA, Japan | |||
05. Sep 22 | 11:00 | 11:30 | 6.1.2 |
ON THE GROWTH OF DISTURBANCES IN A LAMINAR SEPARATION BUBBLE SUBJECTED TO FREESTREAM TURBULENCE Thomas Jaroslawski¹, Olivier Vermeersch¹, Jean-Marc Moschetta², Maxime Forte¹, Erwin Gowree²; ¹ONERA, France ;²ISAE-SUPAERO, France | |||
05. Sep 22 | 11:30 | 12:00 | 6.1.3 |
UNIFORM MOMENTUM ZONES IN A TURBULENT BOUNDARY LAYER OVER PERFORATED WALLS F. Scarano, ISAE - SUPAERO, France | |||
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05. Sep 22 | 10:30 | 11:00 | 7.1.1 |
A SEMANTIC KNOWLEDGE BASED ENGINEERING FRAMEWORK FOR THE RAPID GENERATION OF NOVEL AIR VEHICLE CONFIGURATIONS Jacopo Zamboni¹, Arthur Zamfir¹, Erwin Moerland¹, Björn Nagel¹; ¹German Aerospace Center (DLR), Germany | |||
05. Sep 22 | 11:00 | 11:30 | 7.1.2 |
RULE-BASED VERIFICATION OF A GEOMETRIC DESIGN USING THE CODEX FRAMEWORK B. Boden¹, Y. Cabac¹, T. Burschyk¹, B. Nagel¹; ¹DLR, Germany | |||
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05. Sep 22 | 10:30 | 11:00 | 8.1.1 |
AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO AND STRUT-BRACED WINGS Yoann Le Lamer¹, Emmanuel Benard¹, Joseph Morlier, ICA, Université de Toulouse, ISAE-SUPAERO, MINES ALBI, UPS, INSA, France; Ping He, Iowa State University, United States; ¹ISAE-SUPAERO, Université de Toulouse, France | |||
05. Sep 22 | 11:00 | 11:30 | 8.1.2 |
COMPARING REDUCED ORDER MODEL FORMS FOR NONLINEAR DYNAMICAL SYSTEMS D Massegur¹, D Clifford¹, A Da Ronch¹, S Symon¹; ¹University of Southampton, United Kingdom | |||
05. Sep 22 | 11:30 | 12:00 | 8.1.3 |
NUMERICAL INVESTIGATION ON THE DOUBLE TRANSONIC DIP OF SUPERCRITICAL AIRFOIL FLUTTER T Miyake¹, H Terashima¹; ¹Hokkaido University, Japan | |||
Reserve Paper (interactive) | 8.1.R |
A STUDY ON THE AEROELASTICITY OF AIR-TO-AIR MISSLE IN OVER-THE-SHOULDER LAUNCH K. Lu¹, W.-P. Song¹, K. Ye¹, C.-H. Gao¹, S.-Q Han, Sichuan University, China; ¹Northwestern Polytechnical University, China | |||||
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05. Sep 22 | 10:30 | 11:00 | 9.1.1 |
SERIES-HYBRID RETROFIT OF AN XV-15 TILTROTOR AND EMERGENCY PROCEDURE ENERGETIC ANALYSIS Giulio Avanzini, University of Salento, Italy; Giovanni Bernardini¹, Simone Moretti¹; ¹Roma Tre University, Italy | |||
05. Sep 22 | 11:00 | 11:30 | 9.1.2 |
DEVELOPMENT OF A CONTROLS STRATEGY FOR FUEL CELL-POWERED ALL-ELECTRIC AERO ENGINES BASED ON A FHA S. de Graaf¹, S. Kazula¹, L. Enghardt¹; ¹DLR e.V., Germany | |||
05. Sep 22 | 11:30 | 12:00 | 9.1.3 |
TECHNOLOGY DEMONSTRATOR HYBRID POWER SYSTEM FOR NEW GENERATION OF VTOL UNMANNED AERIAL VEHICLES WITH MTOW UP TO 300 KG M. Wojtas¹, P. Wyszkowski¹, P. Kmita¹, R. Praski¹; ¹Lukasiewicz -Institute of Aviation, Poland | |||
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05. Sep 22 | 10:30 | 11:00 | 10.1.1 |
FINITE ELEMENT MODELLING FOR THE DESIGN OF A PROTECTIVE SHIELD FOR A LEADING EDGE TO WITHSTAND BIRD STRIKE EVENTS A. De Luca, University of Campania L. Vanvitelli, Italy | |||
05. Sep 22 | 11:00 | 11:30 | 10.1.2 |
A REDUCED ORDER MODEL FOR FULL-SCALE DRONE COLLISIONS Florian Franke¹, Uli Burger¹, Christian Hühne, German Aerospace Center, Germany; ¹Technische Hochschule Ingolstadt, Germany | |||
05. Sep 22 | 11:30 | 12:00 | 10.1.3 |
HIGH FIDELITY AIRWORTHINESS BIRD AND DRONE IMPACT ANALYSIS OF ON-DEMAND AIR MOBILITY SERVICE AIRCRAFT P. Vaghela¹, H. Raza¹, E. Stumpf, Institute for Aerospace Systems, RWTH Aachen University, Germany; J. Bayandor¹; ¹CRASH Lab, University at Buffalo - The State Univ. of New York, United States | |||
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05. Sep 22 | 10:30 | 11:00 | 11.1.1 |
LANDING SIMULATION OF A HIGH-ALTITUDE PLATFORM WITH SKID-TYPE LANDING GEAR – FLIGHT PROCEDURE, CONTROLLER, AND LOADS Y. J. Hasan¹, N. Fezans¹, A. Voß, DLR, Institute of Aeroelasticity, Germany; ¹DLR, Institute of Flight Systems, Germany | |||
05. Sep 22 | 11:00 | 11:30 | 11.1.2 |
ALTITUDE ESTIMATION BY WIDE-FIELD-INTEGRATION OF OPTIC FLOW Hiromitsu HIRAIWA¹, Mai BANDO¹, Shinji HOKAMOTO¹; ¹Kyushu university, Japan | |||
05. Sep 22 | 11:30 | 12:00 | 11.1.3 |
FIXED-WING UAVS CONTROL WITH MODEL UNCERTAINTIES Dmitry Ignatyev¹, Argyrios Zolotas¹; ¹Cranfield University, United Kingdom | |||
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05. Sep 22 | 10:30 | 11:00 | 12.1.1 |
REAL-TIME CALCULATION AND ADAPTION OF CONFLICT-FREE AIRCRAFT GROUND TRAJECTORIES L. Nöhren¹, M. Schaper¹, L. Tyburzy¹, K. Muth¹; ¹German Aerospace Center (DLR), Germany | |||
05. Sep 22 | 11:00 | 11:30 | 12.1.2 |
DEVELOPING A DEPARTURE QUEUE MODEL TOWARDS INTEGRATED ARRIVAL AND DEPARTURE RUNWAY OPERATION E. Itoh, The University of Tokyo/ENRI, Japan; D. Iwata, The University of Tokyo, Japan; M. Schultz, Bundeswehr University Munich, Germany Presenter: Daiki Iwata, The University of Tokyo | |||
05. Sep 22 | 11:30 | 12:00 | 12.1.3 |
ASSESSMENT AND CONTROL OF ARRIVAL FLOW AND WAITING TIME APPLYING GT/GI/ST+GI TIME-VARYING QUEUEING MODEL Koki Higasa, The University of Tokyo, Japan; Eri Itoh, Electronic Navigation Research Institute, Japan | |||
Reserve Paper | 12.1.R |
QUANTUM ARRIVAL AND DEPARTURE MANAGEMENT Yoshikawa Nobuyuki, Mitsubishi Electric, Japan | |||||
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05. Sep 22 | 10:30 | 11:00 | 13.1.1 |
LONG TOUCHDOWN THROUGH A SAFETY-II PERSPECTIVE C. Reiser, Embraer, Brazil; E. Villani¹, M. Machado Cardoso Junior¹; ¹ITA, Brazil Presenter: Moacyr Machado Cardoso Junior, ITA | |||
05. Sep 22 | 11:00 | 11:30 | 13.1.2 |
DECISION LADDER APPLICATION ANALYZING A HELICOPTER EMERGENCY Bruno R. Teixeira¹, Luís G L. de Paula¹, Alexandre C. S. Freitas¹, Raphael G. Cortes², Marcelle Y. D. Ribeiro², Moacyr M. C. Júnior², Emília Vilani²; ¹Brazilian Air Force Flight Test and Research Institute, Brazil ;²Instituto Tecnológico de Aeronáutica , Brazil Presenter: Moacyr Machado Cardoso-Júnior, Aeronautical Institute of Technology | |||
05. Sep 22 | 11:30 | 12:00 | 13.1.3 |
SYSTEM SAFETY-BASED SUSTAINABLE AVIATION FUEL SAFETY ASSESSMENT METHOD AND AIRWORTHINESS CERTIFICATION S Ding, Civil Aviation University of China, China; C Gan¹, T Qiu¹, P Liu¹; ¹Beihang University, China | |||
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05. Sep 22 | 10:30 | 11:00 | 14.1.1 |
OPERATIONAL FEASIBILITY STUDY OF AIR TAXI SERVICE USING EVTOL H. Takizawa¹, Z. LEI¹; ¹Suwa University of Science, Japan | |||
05. Sep 22 | 11:00 | 11:30 | 14.1.2 |
NEW GENERATION SPACE VEHICLE OPERATIONS IN THE UNITED ARAB EMIRATES – AN AIRSPACE AND RISK ASSESSMENT O. Lehmann¹, R. El-Jabi¹, K. Webster¹, A. Rachdi¹; ¹Abu Dhabi University, United Arab Emirates | |||
05. Sep 22 | 11:30 | 12:00 | 14.1.3 |
EQUIVALENT CALCULATION METHOD OF FLYOVER NOISE LEVEL OF CUTBACK TAKE-OFF FOR CIVIL JET AIRPLANE AIRWORTHINESS CERTIFICAT SONG Yahui¹, ZHANG Xiaoliang¹, LIU Qiuhong, Northwestern Polytechnical University, China; ZHANG Yuelin¹; ¹Chinese Flight Test Establishment, China | |||
Reserve Paper | 14.1.R |
A GLOBAL APPROACH TO ASSESSING THE CLIMATE RESILIENCE OF AIRPORTS M P Osund-Ireland¹, A J Powell¹, C J Ireland¹; ¹susteer AB, Sweden | |||||
Reserve Paper (interactive) | 14.1.R |
THE DIONYSUS PROGRAM: 99942 APOPHIS, TRANS-MARS INJECTION AND SPACE LIFT CONSTRUCTION (99942 AT-MIASLC) A Sanks, United States Air Force Academy, United States |
12:00 - 13:00 | Lunch Break |
0.2 | GL1 “Future Airspace – Meeting Demand Through Integration” Lynne Thompson Hopper, USA Chair: S. Bagassi ICAS EC member | |||
05. Sep 22 | 13:00 | 14:00 |
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05. Sep 22 | 14:10 | 14:40 | 1.2.1 |
A ROADMAP TOWARDS AN ENVIRONMENTALLY SUSTAINABLE AVIATION MARKETPLACE B Loxton, MAGNIX, United States | |||
05. Sep 22 | 14:40 | 15:10 | 1.2.2 |
HYBRID ELECTRIC PROPULSION DEVELOPMENT FOR COMMERCIAL AVIATION C. Andrews, GE, United States Presenter: Christine Andrews, GE | |||
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05. Sep 22 | 14:10 | 14:40 | 2.2.1 |
MULTIDISCIPLINARY DESIGN OF AN ADVANCED EMPENNAGE AND REAR FUSELAGE CONCEPT FOR A COMMERCIAL AIRCRAFT R.C. Llamas-Sandin¹, C.D. Handal-Rivera¹; ¹Airbus OSL, Spain | |||
05. Sep 22 | 14:40 | 15:10 | 2.2.2 |
SYSTEMS ARCHITECTING A PRACTICAL EXAMPLE OF DESIGN SPACE MODELING AND SAFETY-BASED FILTERING WITHIN THE AGILE 4.0PROJECT A.K. Jeyaraj¹, J.H. Bussemaker², S. Liscouët-Hanke¹, L. Boggero²; ¹Concordia University, Canada ;²DLR, Germany | |||
05. Sep 22 | 15:10 | 15:40 | 2.2.3 |
AN EFFICIENT SOLUTION FOR AERODYNAMIC SHAPE OPTIMIZATION WITHIN THE MID-RANGE APPROXIMATION FRAMEWORK Y. ZHANG¹, F. QU¹, J. Q. BAI¹, D. S. JIA², E. K. Bontoft², V. V. Toropov²; ¹Northwestern Polytechnical University, China ;²Queen Mary University of London, United Kingdom | |||
Reserve Paper | 2.2.R |
EFFICIENT SURROGATE-BASED MULTI-OBJECTIVE OPTIMIZATION ALGORITHM WITH A NEW ADAPTIVE WEIGHT VECTORS GENERATION Z. Lu¹, Z.-H. Han¹, Z. Zhou, Science and Technology on Scramjet Laboratory,CARDC, China; W.-P. Song¹, Y. Zhang¹; ¹Northwestern Polytechnical University, China | |||||
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05. Sep 22 | 14:10 | 14:40 | 3.2.1 |
UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIO Andrew Gomes P. Sarmento ¹, Thiago Rosado de Paula ¹, Emilia Villani ², Abner Souza Oliveira ², Moacyr Machado Cardoso ², Henrique Costa Marques ²; ¹Aeronautics Institute of Technology, Brazil ;²Aeronautics Institute of Technology , Brazil Presenter: Emilia Villani , Aeronautics Institute of Technology | |||
05. Sep 22 | 14:40 | 15:10 | 3.2.2 |
RESEARCH ON THE OVERALL DESIGN OF A HIGH-SPEED MORPHING UAV C. Ding, School of Aeronautic Science and Engineering,Beihang University, China; T.-L. Ma, Institute of Unmanned System, Beihang University, China; J.-C. Fu, School of Transportation ScienceandEngineering,BeihangUniversity, China; X.-S. Wang, School of Aeronautic Science and Engineering, Beihang University, China | |||
05. Sep 22 | 15:10 | 15:40 | 3.2.3 |
MULTIDISCIPLINARY DESIGN OPTIMIZATION OF A LOW OBSERVABLE UAV Muhammad Shafique, Insitute of Space Technology, Pakistan; Dr. Syed Hussein Raza Hamadani¹, Sohaib Khan¹, Taimoor Jan Durrani¹; ¹Institute of Space Technology, Pakistan | |||
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05. Sep 22 | 14:10 | 14:40 | 4.2.1 |
VALIDATION STUDY OF BLUNTED AND SHARP CONES AT HYPERSONIC SPEED E. K. T. Carias¹, S. A. Prince¹; ¹Cranfield University, United Kingdom | |||
05. Sep 22 | 14:40 | 15:10 | 4.2.2 |
AERODATABASE DEVELOPMENT AND INTEGRATION OF HYPERSONIC CRUISER VEHICLES IN MORE&LESS PROGRAM P. Roncioni¹, M. Marini¹, R. Fusaro², N. Viola²; ¹CIRA, Italy ;²POLITO, Italy | |||
05. Sep 22 | 15:10 | 15:40 | 4.2.3 |
TURBULENCE MODELLING STUDIES OF SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS ON HIFIRE-1 AXISYMMETRIC CONE CYLINDER FLARE FA Maulana, Bandung Institute of Technology, Indonesia | |||
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05. Sep 22 | 14:10 | 14:40 | 5.2.1 |
THE GROUP OF RESPONSABLES “FLIGHT MECHANICS, SYSTEMS AND INTEGRATION”: AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES Bernd Korn, DLR, Germany; Martin Hagström, FOI, Sweden | |||
05. Sep 22 | 14:40 | 15:10 | 5.2.2 |
• THE GROUP OF RESPONSABLES “ROTORCRAFT (GOR RC)”: AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES Antonio Visingardi, CIRA, Italy; Rainer Heger, Airbus Helicopters, Germany; Arnaud Le Pape, ONERA, France; Richard Markiewicz, DSTL, United Kingdom; Barbara Ohlenforst, NLR, Netherlands; Klausdieter Pahlke, DLR, Germany; Mark White, University of Liverpool, United Kingdom | |||
05. Sep 22 | 15:10 | 15:40 | 5.2.3 |
AVIATION SECURITY CONCERNS Angela Vozella, Italian Aerospace Research Centre, Italy; Pierre Bieber, ONERA, France | |||
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05. Sep 22 | 14:10 | 14:40 | 6.2.1 |
STRAKE SECTION IMPACT ON HYBRID-DELTA-WING AERODYNAMICS D. Sedlacek, Technical University of Munich, Germany | |||
05. Sep 22 | 14:40 | 15:10 | 6.2.2 |
VOLUMETRIC VELOCITY MEASUREMENTS OF A HELICAL VORTEX PAIR Dominic Schröder¹, Thomas Leweke, CNRS, Aix-Marseille Université, Centrale Marseille, France; Ralf Hörnschemeyer¹, Eike Stumpf¹; ¹Institute of Aerospace Systems, RWTH Aachen University, Germany | |||
05. Sep 22 | 15:10 | 15:40 | 6.2.3 |
CFD AND EXPERIMENTS ON THE DLR-F23 COMBAT AIRCRAFT WIND TUNNEL MODEL J. Zastrow¹, F. Oberdieck¹, U. Henne¹, C. Klein¹; ¹DLR - German Aerospace Center, Germany | |||
Reserve Paper (interactive) | 6.2.R |
INFLUENCE OF TIP DIHEDRAL ON ROTOR AERODYNAMIC PERFORMANCE AND TIP VOTEX M.-H. Kang¹, X. Zhao¹, R. Yao¹, H.-Y. Li¹; ¹Norhwestern Polytechnical University, China Presenter: Hongyan Li, Norhwestern Polytechnical University | |||||
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05. Sep 22 | 14:10 | 14:40 | 7.2.1 |
ASSESSMENT OF THE SUSTAINABILITY OF THE IMPLEMENTATION OF CIRCULAR ECONOMY PRINCIPLES IN PRODUCING AIRCRAFT STRUCTURES Dionysios Markatos¹, Spiros Pantelakis¹; ¹University of Patras, Greece Presenter: Dionysios Markatos | |||
05. Sep 22 | 14:40 | 15:10 | 7.2.2 |
INVESTIGATION ON INTEGRATING RECYCLABILITY AS A FUNCTION AT THE DESIGN PHASE OF COMPLEX-LOADED STRUCTURAL COMPONENTS A. Filippatos¹, K. Abhyankar, Institute of Lightweight Engineering and Polymer Technology, Tec, Germany; G. Tzortzinis¹; ¹Dresden Center for Intelligent Materials (DCIM), Technische Univ, Germany | |||
05. Sep 22 | 15:10 | 15:40 | 7.2.3 |
SIGMOIDAL SENSING DEVICES FOR MONITORING TO IMPROVE MAINTENANCE OPERATIONS IN AERONAUTICS Helge Pfeiffer¹, Hans Sekler, Deutsche Lufthansa AG, Germany; Martine Wevers¹; ¹KU Leuven, Belgium | |||
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05. Sep 22 | 14:10 | 14:40 | 8.2.1 |
XRF1 HIGH LIFT LOAD ANALYSIS OF WING AND HIGH LIFT SYSTEM S. Pülm¹, V. Handojo¹, R. B. Seidler¹; ¹German Aerospace Center (DLR), Germany Presenter: Sven Pülm, German Aerospace Center (DLR) | |||
05. Sep 22 | 14:40 | 15:10 | 8.2.2 |
AEROELASTIC STABILITY ANALYSIS OF THE HAMMERHEAD LAUNCH VEHICLE USING CFD-CAE COUPLED METHOD IN THE TRANSONIC REGION H.G. Rho, Korea Aerospace Univeristy, South Korea; J.S. Bae¹, S.H. Park, Konkuk University, South Korea; P.-A. Nguyen¹; ¹Korea Aerospace University, South Korea | |||
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05. Sep 22 | 14:10 | 14:40 | 9.2.1 |
ASSESSMENT OF A SERIAL COOLING CONCEPT FOR HTPEM FUEL CELL SYSTEMS FOR AVIATION APPLICATIONS A. Link¹, J. Ludowicy¹, M. Staggat¹; ¹German Aerospace Center (DLR), Germany | |||
05. Sep 22 | 14:40 | 15:10 | 9.2.2 |
LITHIUM-ION BATTERY HAZARD IDENTIFICATION AND SAFETY RISK MANAGEMENT IN AIRCRAFT WITH ELECTRIC PROPULSION T. Raoofi¹, M. Yildiz, Erciyes university, Turkey; S. Tolun¹; ¹University of Kyrenia, Turkey | |||
05. Sep 22 | 15:10 | 15:40 | 9.2.3 |
DEMONSTRATION FLIGHTS OF HYBRID ELECTRIC AIRCRAFT P. Bohnert, United Kingdom; S. X. Ying, United States; M. Selier, Netherlands | |||
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05. Sep 22 | 14:10 | 14:40 | 10.2.1 |
MACHINE LEARNING METHODS ENSURING BOTH PERFORMANCE AND INTERPRETABILITY OF ESTIMATING AIRCRAFT ARRIVAL TIMES N. Morikawa, Faculty of Aerospace Engineering, The University of Tokyo, Japan; E. Itoh, Air Traffic Management Department, Electronic Navigation Researc, Japan | |||
05. Sep 22 | 14:40 | 15:10 | 10.2.2 |
APPLYING MACHINE LEARNING FOR TAXI-TIME PREDICTION AT TOKYO INTERNATIONAL AIRPORT E. Itoh, The University of Tokyo, Japan | |||
05. Sep 22 | 15:10 | 15:40 | 10.2.3 |
AN AUCTION-BASED MECHANISM FOR A PRIVACY-PRESERVING MARKETPLACE FOR ATFM SLOTS C. G. Schuetz, Johannes Kepler University Linz, Austria; S. Ruiz, EUROCONTROL Innovation Hub, France; E. Gringinger¹, C. Fabianek¹, Thomas Loruenser, AIT Austrian Institute of Technology, Austria; ¹Frequentis AG, Austria | |||
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05. Sep 22 | 14:10 | 14:40 | 11.2.1 |
EXPECTED TEAMWORK ATTRIBUTES BETWEEN HUMAN OPERATOR AND AUTOMATION IN AIR TRAFFIC CONTROL Å Svensson, LFV, Sweden; N Rönnberg, Linköping University, Sweden | |||
05. Sep 22 | 14:40 | 15:10 | 11.2.2 |
HANDLING QUALITIES RATING SCALE THE IMPACT OF THE PILOT SUBJECTIVITY IN WORKLOAD EVALUATION Mariane D. Turaça, Universidade de São Paulo, Brazil | |||
05. Sep 22 | 15:10 | 15:40 | 11.2.3 |
PILOT’S ATTENTION DISTRIBUTION MODELING USING HIDDEN MARKOV MODELS Jiri Hanak¹, Jan Vlk¹, Peter Chudy¹; ¹Brno University of Technology, Czech Republic | |||
Reserve Paper | 11.2.R |
EXPLORATORY STUDY OF MENTAL WORKLOAD IN HELICOPTER AIR-TO-GROUND ROCKET FIRING R. G. Cortes¹, E. Villani¹, M. M. Cardoso Júnior¹; ¹Aeronautics Institute of Technology, Brazil Presenter: Emilia Villani, Aeronautics Institute of Technology | |||||
Reserve Paper | 11.2.R |
STRESSING SAFETY ASSESSMENT METHODS BY HIGHER LEVELS OF AUTOMATION L. Meyer¹, C. Bjursten Carlsson¹, Å. Svensson¹, M. Peukert¹, L. Danielson, SDATS, Sweden; B. Josefsson¹; ¹LFV, Sweden | |||||
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05. Sep 22 | 14:10 | 14:40 | 12.2.1 |
DIGITAL TWIN CAPABILITIES AND CHALLENGES IN THE CONTEXT OF IVHM IN AVIATION M. Castaño Arranz, Luleå University of Technology, Sweden | |||
05. Sep 22 | 14:40 | 15:10 | 12.2.2 |
OPERABILITY PROJECTION OF MAJOR AIRCRAFT COMPONENTS DURING EARLY AIRCRAFT DESIGN S. S. MANIKAR, Airbus/ ISAE-SUPAERO, France; J. JEZEGOU¹, P. de SAQUI-SANNES¹, P. ASSEMAN, Airbus, France; E. BENARD¹; ¹ISAE-SUPAERO, France | |||
05. Sep 22 | 15:10 | 15:40 | 12.2.3 |
DIGITAL TWIN CONCEPT FOR AIRCRAFT COMPONENTS H. Meyer¹, A.-K. Koschlik¹, F. Raddatz¹; ¹German Aerospace Center, Germany | |||
Reserve Paper | 12.2.R |
DESIGNING SUSTAINABLE AVIATION SOLUTIONS WITH DIGITAL TWIN APPROACH M. J. Grundström , Tampere university, Finland | |||||
Reserve Paper (interactive) | 12.2.R |
ESTIMATION OF ROTOR IMBALANCE AND MODEL DISCREPANCY USING A BAYESIAN APPROACH Rahul Rameshbabu¹, Dushhyanth Rajaram¹, Olivia J. Pinon Fischer¹, Dimitri N. Mavris¹; ¹Georgia Institute of Technology, United States |
15:40 - 16:00 | Break |
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05. Sep 22 | 16:00 | 16:30 | 1.3.1 |
A MULTIFIDELITY MULTIDISCIPLINARY APPROACH TO UNCONVENTIONAL AIRCRAFT DEVELOPMENT AND ASSESSMENT WITH APPLICATIONS D. W. Zingg, University of Toronto Institute for Aerospace Studies, Canada | |||
05. Sep 22 | 16:30 | 17:00 | 1.3.2 |
OVERVIEW OF AERODYNAMIC DESIGN ACTIVITIES PERFORMED AT ONERA TO REDUCE AVIATION\'S CLIMATE IMPACT M. Méheut¹, G. Arnoult¹, O. Atinault¹, Q. Bennehard¹, C. Francois¹; ¹ONERA, France | |||
05. Sep 22 | 17:00 | 17:30 | 1.3.3 |
MDAO OF A TRANSONIC TRUSS-BRACED WING VISION VEHICLE N. A. Harrison, the Boeing Co., United States | |||
05. Sep 22 | 17:30 | 18:00 | 1.3.4 |
APPLICATION OF AERODYNAMICS AND AERO-STRUCTURAL OPTIMIZATION FOR ENERGY EFFICIENT AIRCRAFT O Brodersen, Germany | |||
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05. Sep 22 | 16:00 | 16:30 | 2.3.1 |
VALIDATION OF SCALED FLIGHT TESTING P. Schmollgruber, ONERA, France | |||
05. Sep 22 | 16:30 | 17:00 | 2.3.2 |
TECHNOLOGY INTEGRATION FOR FUTURE AIRCRAFT CONFIGURATIONS D Reckzeh, Airbus, Germany | |||
05. Sep 22 | 17:00 | 17:30 | 2.3.3 |
MARKET ANALYSIS, TLARS SELECTION AND PRELIMINARY DESIGN INVESTIGATIONS FOR A REGIONAL HYBRID-ELECTRIC AIRCRAFT V. Marciello¹, M. Ruocco, SmartUp Engineering s.r.l., Italy; F. Nicolosi¹, M. Di Stasio¹; ¹University of Naples Federico II, Italy | |||
05. Sep 22 | 17:30 | 18:00 | 2.3.4 |
UNMANNED AEW/ISR PLATFORM CONCEPTUAL DESIGN AND TECHNOLOGY ASSESSMENT K. Amadori, Saab Aeronautics, Sweden; M. Emeneth, PACE America Inc., United States; A. Papageorgiou, Linköpings University, Sweden | |||
Reserve Paper (interactive) | 2.3.R |
INVENTIVE PROBLEM-SOLVING PRINCIPLES APPLIED TO DECISION-MAKING PROCESS OF PRODUCTS PLATFORM P.B. Barros Soares, Embraer S.A., Brazil | |||||
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05. Sep 22 | 16:00 | 16:30 | 3.3.1 |
A COMMON FRAMEWORK FOR THE DESIGN OPTIMIZATION OF FIXED-WING, MULTICOPTER AND VTOL UAV CONFIGURATIONS F. Pollet¹, S. Delbecq¹, M. Budinger, ICA, Université de Toulouse, ISAE-SUPAERO, MINES ALBI, UPS, INSA, France; J.-M. Moschetta¹, J. Liscouët, Concordia University, Canada; ¹ISAE-SUPAERO, France | |||
05. Sep 22 | 16:30 | 17:00 | 3.3.2 |
DESIGN OF A HALE UAV FOR ATMOSPHERIC IMAGING V. Nan Fernandez-Ayala¹, L. Vimláti¹, A. Matoses Gimenez¹, H. Delmotte¹, M. Ivchenko¹, R. Mariani¹; ¹KTH Royal Institute of Technology, Sweden | |||
05. Sep 22 | 17:00 | 17:30 | 3.3.3 |
ENHANCING UAS DESIGN PROCESS FOR SPECIFIC CATEGORY OPERATIONS USING SORA. R. Kalra¹, P. Flores-Peña, Drone Hopper S.L., Spain; A. Sanchez-Carmona¹, C. Cuerno-Rejado¹; ¹Universidad Politécnica de Madrid, Spain | |||
05. Sep 22 | 17:30 | 18:00 | 3.3.4 |
OPENVSP BASED AERODYNAMIC DESIGN OPTIMIZATION TOOL BUILDING METHOD AND ITS APPLICATION TO TAILLESS UAV J. Kim¹, T. Tsuchiya¹; ¹The University of Tokyo, Japan | |||
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05. Sep 22 | 16:00 | 16:30 | 4.3.1 |
MODEL-BASED PERFORMANCE EVALUATION OF AIRCRAFT ACTUATOR TECHNOLOGIES F Larsson¹, C Reichenwallner², A Dell'Amico¹, P Krus²; ¹Saab AB, Sweden ;²Linköping University, Sweden | |||
05. Sep 22 | 16:30 | 17:00 | 4.3.2 |
A COMPARATIVE ANALYSIS OF INNOVATIVE DIGITAL HYDRAULIC ACTUATORS FOR PRIMARY FLIGHT CONTROL R. Simões Lopes Junior¹, D. Oliveira e Silva¹, M. P. Nostrani¹, A. Dell´Amico, Saab AB, Sweden; P. Krus, Linköping University, Sweden; V. J. De Negri¹; ¹Federal University of Santa Catarina, Brazil | |||
05. Sep 22 | 17:00 | 17:30 | 4.3.3 |
AN EVALUATION METHOD FOR AIRCRAFT ACTUATION SYSTEMS OPERATIONAL COST C Reichenwallner, Linköping university, Sweden; F Larsson¹, A Dell'Amico¹; ¹Saab AB, Sweden | |||
05. Sep 22 | 17:30 | 18:00 | 4.3.4 |
DEVELOPMENT OF A HIGH EFFICIENT HYDRAULIC POWER PACK L.Z. Lima¹, M.N. Duval¹, T. Zantner¹, D. Metzler¹, T. Lammering¹, F. Thielecke², N. Trochelmann², P.S. Bischof²; ¹Liebherr-Aerospace Lindenberg GmbH, Germany ;²Hamburg University of Technology, Germany Presenter: Leonardo Zanetti de Lima | |||
Reserve Paper | 4.3.R |
USING EXISTING HARDWARE IN THE EARLY CONCEPT PHASE OF FLIGHT CONTROL ACTUATION SYSTEM DESIGN A. Dell'Amico, Sweden | |||||
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05. Sep 22 | 16:00 | 16:30 | 5.3.1 |
FLYZERO: THE UK VISION FOR ZERO-CARBON EMISSION AIR TRAVEL D J Debney, Aerospace Technology Institute, United Kingdom | |||
05. Sep 22 | 16:30 | 17:00 | 5.3.2 |
IMPACT OF NASCENT TECHNOLOGIES ON THE SUSTAINABILITY ATTRIBUTES OF AN EVOLUTIONARY SINGLE-AISLE AIRCRAFT N.J. Allen, Aerospace Technology Institute, United Kingdom; M.R. Schofield, Ellondee Ltd, United Kingdom | |||
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05. Sep 22 | 15:30 | 16:00 | 6.3.1 |
NUMERICAL AND EXPERIMENTAL STRUCTURAL CHARACTERIZATION OF COMPOSITE ADVANCED JOINT FOR ULTRA LIGHT AEROSPACE PLATFORMS A. Polla, Politecnico di Torino; Royal Melbourne Institute of Technology, Italy; G. Frulla¹, E. Cestino¹, R. Das², P. Marzocca²; ¹Politecnico di Torino, Italy ;²Royal Melbourne Institute of Technology, Australia Presenter: Enrico Cestino, Politecnico di Torino | |||
05. Sep 22 | 16:00 | 16:30 | 6.3.2 |
COMPARISON OF SCARF REPAIR AND SCARF JOINT PERFORMANCE UNDER TENSILE LOAD CONSIDERING THE EFFECT OF STACKING SEQUENCE S Tashi, Sharif University of Technology, Iran | |||
05. Sep 22 | 16:30 | 17:00 | 6.3.3 |
DAMAGE RECOGNITION OF COMPOSITE STRUCTURES BASED ON DOMAIN ADAPTIVE MODEL Shuaishuai Lyu, China | |||
05. Sep 22 | 17:30 | 18:00 | 6.3.4 |
APPLICATION OF THE VIRTUAL CRACK CLOSURE TECHNIQUE FOR CRACKS IN BUILT-UP PANELS W. R. P. Mendonca¹, M. R. B. Rodrigues¹; ¹Embraer S.A., Brazil Presenter: Willy Mendonca, Embraer S.A. | |||
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05. Sep 22 | 16:00 | 16:30 | 7.3.1 |
WIND TUNNEL EXPERIMENT WITH AN EPP-WING TO INVESTIGATE AEROELASTIC EFFECTS OF NONLINEAR ELASTIC STIFFNESSES K. Bramsiepe¹, M. Braune¹, W. Krüger¹, L. Tichy¹; ¹DLR - Institute of Aeroelasticity, Germany | |||
05. Sep 22 | 16:30 | 17:00 | 7.3.2 |
DESIGN OF AN INNOVATIVE WING TIP FOR AEROELASTIC CONTROL: FROM SCRATCH TO FLIGHT TEST Francesco Toffol¹, Federico Fonte, Leonardo Helicopters, Italy; Sergio Ricci¹; ¹Politecnico di Milano, Italy | |||
05. Sep 22 | 17:00 | 17:30 | 7.3.3 |
LONGITUDINAL DYNAMICS IDENTIFICATION OF A FLEXIBLE UAV P. Fernandes, Brazil | |||
05. Sep 22 | 17:30 | 18:00 | 7.3.4 |
EVALUATION ENVIRONMENT FOR CASCADED AND PARTLY DECENTRALIZED MULTI-RATE LOAD ALLEVIATION CONTROLLERS C. Wallace¹, S. Schulz¹, N. Fezans¹, T. Kier¹, G. Weber, Liebherr-Aerospace, Germany; ¹German Aerospace Center (DLR), Germany | |||
Reserve Paper | 7.3.R |
SOME EXPERIMENTAL RESULTS ON DYNAMIC AEROELASTICITY OF PLATES AND SHELLS IN SUBSONIC AND SUPERSONIC FLOW. J. Lübker, Germany | |||||
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05. Sep 22 | 16:00 | 16:30 | 8.3.1 |
A COMPARITIVE ASSESSMENT OF MULTI-OBJECTIVE OPTIMISATION METHODOLOGIES FOR AERO-ENGINE NACELLES A. Swarthout¹, D. MacManus¹, F. Tejero¹, J. Matesanz-Garcia¹, L. Boscagli¹, C. Sheaf, Rolls Royce Plc., United Kingdom; ¹Cranfield University, United Kingdom | |||
05. Sep 22 | 16:30 | 17:00 | 8.3.2 |
KNOWLEDGE-BASED CONCEPTUAL DESIGN METHODS FOR GEOMETRY AND MASS ESTIMATION OF RUBBER AERO ENGINES J. Häßy¹, J. Schmeink¹; ¹DLR, Germany | |||
05. Sep 22 | 17:00 | 17:30 | 8.3.3 |
COUPLED AEROPROPULSIVE ANALYSIS AND OPTIMIZATION OF A HIGH BYPASS TURBOFAN ENGINE A. H. R. Lamkin¹, A. Yildirim¹, J. R. R. A. Martins¹; ¹University of Michigan, United States | |||
Reserve Paper (interactive) | 8.3.R |
MULTIDISCIPLINARY OPTIMIZATION OF COMBUSTION CHAMBER FOR SMALL GAS TURBINE ENGINES Cong-Anh Pham¹, Quang-Hai Nguyen¹, Tuan-Anh Vu¹, Nhu-Van Nguyen¹, Phi-Minh Nguyen¹; ¹Viettel Aerospace Institute, Viettel Group, Vietnam Presenter: Nhu-Van Nguyen, Viettel Aerospace Institute, Viettel Group | |||||
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05. Sep 22 | 16:00 | 16:30 | 9.3.1 |
FLIGHT DYNAMICS SIMULATION AND FCS AUTO-GENERATION IN THE CONCEPTUAL DESIGN PHASE OF AN UNSTABLE SUPERSONIC AIRCRAFT E Johansson¹, P Månsson¹, P Sjöberg¹; ¹Saab Aeronautics, Sweden | |||
05. Sep 22 | 16:30 | 17:00 | 9.3.2 |
VALIDATION OF A HYBRID LOADS OBSERVER FOR A SUBSCALE TEST AIRCRAFT WITH DISTRIBUTED ELECTRIC PROPULSION O. Luderer¹, F. Thielecke¹; ¹Hamburg University of Technology, Germany | |||
05. Sep 22 | 17:00 | 17:30 | 9.3.3 |
A BI-LEVEL CO-DESIGN APPROACH FOR MULTICOPTERS J. MABBOUX¹, S. DELBECQ¹, V. POMMIER-BUDINGER¹, J. BORDENEUVE-GUIBE¹, A. TRUC-HERMEL², J.-M. KAI²; ¹ISAE Supaero, France ;²SAFRAN, France | |||
05. Sep 22 | 17:30 | 18:00 | 9.3.4 |
DEEP REINFORCEMENT LEARNING FOR EVTOL HOVERING CONTROL D.S. Alarcon¹, J. H. Bidinotto¹; ¹University of São Paulo, Brazil | |||
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05. Sep 22 | 16:00 | 16:30 | 10.3.1 |
ATTENTION-BASED RECURRENT NEURAL NETWORK ASSISTED EXTENDED KALMAN FILTER FOR MANEUVERING TARGET TRACKING Dongshik Won¹, Dongwoo Lee¹, Hyochoong Bang¹; ¹KAIST, South Korea | |||
05. Sep 22 | 16:30 | 17:00 | 10.3.2 |
OPTIMAL HOVERING WING KINEMATICS OF FLAPPING-WING MODEL USING REINFORCEMENT LEARNING H.-H. Yang¹, S.-G. Lee¹, Y.-J. Han¹, J.-H. Han¹; ¹Korea Advanced Institute of Science and Technology, South Korea Presenter: Hyeon-Ho Yang, Korea Advanced Institute of Science and Technology | |||
05. Sep 22 | 17:00 | 17:30 | 10.3.3 |
PREFLIGHT DIAGNOSIS OF MULTICOPTER ACTUATOR FAULT USING SUPERVISED LEARNING WITH DISTURBANCE OBSERVER OUTPUTS T.G Kim¹, Y.J Kim¹, S.K Kim¹; ¹Chungnam National University, South Korea | |||
05. Sep 22 | 17:30 | 18:00 | 10.3.4 |
USING DEEP REINFORCEMENT LEARNING TO IMPROVE THE ROBUSTNESS OF UAV LATERAL-DIRECTIONAL CONTROL Rui Wang¹, Zhou Zhou¹, Zhu Xiaoping¹, Zheng Liming, Delft University of Technology, Netherlands; ¹Northwestern Polytechnical University, China | |||
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05. Sep 22 | 16:00 | 16:30 | 11.3.1 |
IMPROVED CONFIGURATION MANAGEMENT FOR GREENER APPROACHES – EVALUATION OF A NOVEL PILOT SUPPORT CONCEPT T. Bauer¹, F. Abdelmoula¹, J. Boyer, Thales, France; M. Gerber, Swiss Sklylab Foundation, Switzerland; J. Meister², J. M. Wunderli²; ¹DLR e.V., Germany ;²Empa, Swiss Fed. Laboratories for Materials Science & Technology, Switzerland | |||
05. Sep 22 | 16:30 | 17:00 | 11.3.2 |
A COMPARISON OF CLIMATE-OPTIMISED AND FUEL-OPTIMISED INTERMEDIATE STOP OPERATIONS FOR SELECTED CASE STUDIES Z. L. Zengerling¹, F. Linke¹, C. Weder¹, Katrin Dahlmann¹; ¹Deutsches Zentrum für Luft- und Raumfahrt, Germany | |||
05. Sep 22 | 17:00 | 17:30 | 11.3.3 |
IMPLICATIONS OF POTENTIAL NEW REGULATORY MEASURES TO ADDRESS AVIATION EMISSIONS A. NIETO¹, G. ALONSO¹, J. CUBAS¹; ¹Universidad Politécnica de Madrid, Spain | |||
05. Sep 22 | 17:30 | 18:00 | 11.3.4 |
AN ENGINELESS TAXI OPERATIONS SYSTEM USING BATTERY-OPERATED AUTONOMOUS TOW TRUCKS S. Zaninotto¹, J. Gauci¹, B. Zammit¹; ¹University of Malta, Malta | |||
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05. Sep 22 | 16:00 | 16:30 | 12.3.1 |
A NOVEL METHOD FOR DETECTING UAVS USING PARALLEL NEURAL NETWORKS WITH RE-INFERENCE H. Stepien, Saab Aeronautics, Sweden; M. Bilger, Saab Surveillance, Sweden; H. Forsberg¹, B. Lindgren, Saab Dynamics, Sweden; J. Hjorth¹; ¹Mälardalen University, Sweden | |||
05. Sep 22 | 16:30 | 17:00 | 12.3.2 |
URBAN AIR TRAFFIC MANAGEMENT FOR COLLISION AVOIDANCE WITH UNCOOPERATIVE AIRSPACE USERS I. Panchal¹, I.C. Metz, German Aerospace Center, Germany; M. Ribeiro, TU Delft, Netherlands; S.F. Armanini¹; ¹TU Munich, Germany | |||
05. Sep 22 | 17:00 | 17:30 | 12.3.3 |
A HUMAN-MACHINE INTERFACE ANALYSIS FOR TELEOPERATION OF UAV OVERTIME DELAY A. G. P. Sarmento¹, T. Rosado de Paula¹, A. S. Oliveira¹, E. T. da Silva¹, J. Possamai¹, H. C. Marques¹, M. M. Cardoso Junior¹, E. Villani¹; ¹Aeronautics Institute of Technology (ITA), Brazil Presenter: Moacyr Machado Cardoso Júnior , Aeronautics Institute of Technology | |||
05. Sep 22 | 17:30 | 18:00 | 12.3.4 |
IMAGE SEGMENTATION BASED EMERGENCY LANDING FOR AUTONOMOUS AND AUTOMATED UNMANNED AERIAL VEHICLES P. Hausmann¹, H. Meeß, Fraunhofer IVI, Germany; G. Elger¹; ¹Technische Hochschule Ingolstadt, Germany | |||
Reserve Paper | 12.3.R |
EVALUATION AND QUANTIFICATION OF THE POTENTIAL CONSEQUENCES OF BIRD STRIKES IN URBAN AIR MOBILITY A. Devta¹, I. C. Metz, DLR, Germany; S. F. Armanini¹; ¹Technical University of Munich, Germany | |||||
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05. Sep 22 | 16:00 | 16:30 | 13.3.1 |
THE ALBATROSS PROJECT – A EUROPEAN INITIATIVE TO REDUCE AVIATION’S CARBON DIOXIDE EMISSIONS IN LARGE SCALE Falk Sachs¹, Fethi Abdelmoula¹, Dennis Vechtel¹; ¹DLR, Germany Presenter: Dennis Vechtel, DLR | |||
05. Sep 22 | 16:30 | 17:00 | 13.3.2 |
ZERO-EMISSION REGIONAL AVIATION IN SCANDINAVIA R. T. Sorrentino¹, R. C. Parello¹, M. Delage¹, C. Y. Justin¹, D. N. Mavris¹, C. Jouannet², K. Amadori²; ¹Georgia Institute of Technology, United States ;²Saab AB/Saab Aeronautics, Sweden Presenter: Robbie Sorrentino, Georgia Institute of Technology | |||
05. Sep 22 | 17:00 | 17:30 | 13.3.3 |
PERFORMANCE EVALUATION OF THE ARRIVAL OPERATIONS IN TERMINAL AREA H Hardell¹, A Lemetti¹, T Polishchuk¹; ¹Linköping University, Sweden | |||
05. Sep 22 | 17:30 | 18:00 | 13.3.4 |
AERODYNAMIC INVESTIGATION OF VERY CLOSELY FLYING FIGHTERS TO DEVELOP NEW FORMATION TYPES Süleyman Mert Aydin¹, Abdurrahman Gazi Yavuz, Turkish Aerospace Industries, Turkey; Mustafa Kaya¹; ¹Yildirim Beyazit University, Turkey | |||
Reserve Paper | 13.3.R |
DATA-DRIVEN APPROACH TO OPTIMAL AIRCRAFT MAINTENANCE O.C Okoro¹, M Zaliskyi¹, D Serhii , National Aviation University , Ukraine; S Qudus, Tamara Niger Aviation, Niger; ¹National Aviation University, Ukraine |