
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.
Tuesday, 06. Sep 2022
0.1 | GL 2 “Towards Certification by Analysis for Flight Characteristics” Robert Gregg III , USA Chair: F. Collier ICAS EC member | |||
06. Sep 22 | 08:00 | 09:00 |
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0.2 | Interactive Presentations (Coffee will be served after 10:00) Chair: O. Pinon Fischer ICAS PC Member | |||
06. Sep 22 | 09:00 | 10:30 |
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06. Sep 22 | 10:30 | 11:00 | 2.1.1 |
AERODYNAMIC SHAPE OPTIMIZATION OF CRM WING VIA DEEP LEARNING-ASSISTED GENETIC ALGORITHM M. A. Hariansyah¹, K. Shimoyama¹; ¹Institute of Fluid Science, Tohoku University, Japan | |||
06. Sep 22 | 11:00 | 11:30 | 2.1.2 |
SUCCESSIVE KNOWLEDGE BUILDUP AND TRANSFER DURING THE ANALYSIS OF SCALED UAV WINGS BY MEANS OF MACHINE LEARNING T. Klaproth¹, M. Hornung¹; ¹Technical University of Munich, Germany | |||
06. Sep 22 | 11:30 | 12:00 | 2.1.3 |
AIRCRAFT DESIGN PARAMETER ESTIMATION USING DATA-DRIVEN MACHINE LEARNING MODELS S. Shin¹, S. Lee¹, C. Son, Cheongju University, South Korea; K. Yee, Seoul National University, South Korea; ¹Korea Institute of Industrial Technology, South Korea | |||
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06. Sep 22 | 10:30 | 11:00 | 3.1.1 |
EXPLORATION OF BOX-WING CONCEPT USING AERODYNAMIC SHAPE OPTIMIZATION P. D. Bravo-Mosquera¹, T Chau², F Catalano¹, D Zingg²; ¹University of São Paulo, Brazil ;²University of Toronto, Canada | |||
06. Sep 22 | 11:00 | 11:30 | 3.1.2 |
CONCEPTUAL STUDY OF HYBRID-ELECTRIC BOX-WING AIRCRAFT TOWARD THE REDUCTION OF AVIATION EFFECTS ON LOCAL AIR QUALITY [..] K. Abu Salem¹, V. Cipolla¹, G. Palaia¹, V. Binante², D. Zanetti²; ¹University of Pisa, Italy ;²SkyBox Engineering, Italy Presenter: Karim Abu Salem, University of Pisa, Dep. of Civil and Industrial Engineering | |||
06. Sep 22 | 11:30 | 12:00 | 3.1.3 |
MULTIDISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION PROCESS DEDICATED TO BLENDED WING BODY CONFIGURATIONS J. Gauvrit-Ledogar¹, A. Tremolet¹, F. Moens¹, M. Méheut¹, S. Defoort¹, R. Liaboeuf¹, F. Morel¹, B. Paluch¹; ¹ONERA, France | |||
Reserve Paper | 3.1.R |
RESEARCH ON THE SELECTION METHOD OF TYPICAL RCS BENCHMARK BASED ON AHP Yu-Lu Huang¹, Wei Du¹, Dao-Qin Huang¹, Jia Liu, Beihang University, China; ¹AVIC CHENGDU AIRCRAFT INDUSTRIAL(GROUP) CO.LTD, China | |||||
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06. Sep 22 | 10:30 | 11:00 | 4.1.1 |
WING BUFFET PRESSURE LOAD PREDICTION BASED ON A HYBRID DEEP LEARNING MODEL R. Zahn¹, A. Weiner, Technical University of Braunschweig, Germany; C Breitsamter¹; ¹Technical University of Munich (TUM), Germany | |||
06. Sep 22 | 11:00 | 11:30 | 4.1.2 |
MACHINE LEARNING FOR AERODYNAMICS PREDICTION Rodrigo Castellanos¹, Alejandro Gorgues¹, Jaime Bowen¹, Esther Andrés¹; ¹INTA, Spain Presenter: Rodrigo Castellanos, INTA | |||
06. Sep 22 | 11:30 | 12:00 | 4.1.3 |
EFFICIENT UNCERTAINTY QUANTIFICATION VIA MULTI-FIDELITY POLYNOMIAL CHAOS-KRIGING METAMODELLING TECHNOLOGY Zhao Huan, Sun Yat-Sen University, China; Gao Zhenghong¹, Xia Lu¹; ¹Northwestern Polytechnical University, China Presenter: Huan ZHAO, SUN YAT-SEN UNIVERSITY | |||
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06. Sep 22 | 10:30 | 11:00 | 5.1.1 |
TRANSITIONAL FLOW MODELLING OF A HYBRID LAMINAR FLOW CONTROL AND VARIABLE CAMBER TRANSONIC TRANSPORT AIRCRAFT WING M. Jentys¹, C. Breitsamter¹; ¹Technical University of Munich, Germany | |||
06. Sep 22 | 11:00 | 11:30 | 5.1.2 |
REACTIVE CONTROL OF BYPASS TRANSITION IN A WING BOUNDARY LAYER José M. Faúndez Alarcón¹, Kenzo Sasaki¹, Ardeshir Hanifi¹, Roger Larsson, Saab Aeronautics, Sweden; Dan S. Henningson¹; ¹KTH Royal Institute of Technology, Linné FLOW Centre, Sweden | |||
06. Sep 22 | 11:30 | 12:00 | 5.1.3 |
DIRECT NUMERICAL SIMULATIONS OF THE EFFECTS OF ROTATION ON A THICK AIRFOIL T. Coelho Leite Fava¹, D. Henningson¹, A. Hanifi¹; ¹KTH, Sweden | |||
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06. Sep 22 | 10:30 | 11:00 | 6.1.1 |
ANALYSIS OF THE EFFECT OF FLOW TRANSITION OVER THE WINGS OF THE BLADE DEMONSTRATOR R Larsson, Saab Aeronautics, Sweden | |||
06. Sep 22 | 11:00 | 11:30 | 6.1.2 |
TO CFD OR NOT TO CFD? COMPARING RANS AND VISCOUS PANEL METHODS FOR AIRFOIL SHAPE OPTIMIZATION E. J. Adler¹, A. C. Gray¹, J. R. R. A. Martins¹; ¹University of Michigan, United States | |||
06. Sep 22 | 11:30 | 12:00 | 6.1.3 |
PUSHER PROPELLER INFLUENCE ON A LAMINAR WING TRANSITION LOCATION USING INFRARED THERMOGRAPHY J. P. Eguea¹, G. P. G. Silva¹, F. M. Catalano¹; ¹USP, Brazil | |||
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06. Sep 22 | 10:30 | 11:00 | 7.1.1 |
EFFECT OF NITRIDING ON MICROSTRUCTURE AND MECHANICAL PROPERTIES ON A TI64 ALLOY FOR AEROSPACE APPLICATIONS S Stekovic¹, R. Romero-Ramirez¹, P. Östlund, NewSoTech AB, Germany; ¹Linköping University, Sweden Presenter: Rodger Romero-Ramirez, Linköping University | |||
06. Sep 22 | 11:00 | 11:30 | 7.1.2 |
MECHANICAL CHARACTERIZATION OF A COMPOSITE STRUCTURAL BATTERY LAMINATE G. M. DI MAURO¹, R. M. RUSSO, Institute for Polymers, Composites and Biomaterials, C.N.R., Italy; G. M. GUIDA¹; ¹University of Naples Federico II – Department of Industrial Eng., Italy | |||
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06. Sep 22 | 10:00 | 10:30 | 8.1.1 |
TOPOLOGY OPTIMIZATION OF COMPLIANT TRAILING EDGE AIRFOIL WITH A PATH-FOLLOWING EQUILIBRIUM SOLUTION C. E. de Souza, Federal University of Santa Maria, Brazil | |||
06. Sep 22 | 10:30 | 11:00 | 8.1.2 |
MORPHING FORWARD WING SECTION SKIN DESIGN FOR A SAILPLANE CONSIDERING WING BENDING Fabian Sturm¹, Mirko Hornung¹; ¹Technical University of Munich, Germany | |||
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06. Sep 22 | 10:30 | 11:00 | 9.1.1 |
DEVELOPMENT OF A CONCEPTUAL DESIGN TOOL TO PREDICT PERFORMANCE OF HYDROGEN FUELLED PRECOOLED AIRBREATHING ROCKET ENGINES G. Grimaldi, Politecnico di Torino, Italy | |||
06. Sep 22 | 11:00 | 11:30 | 9.1.2 |
LARGE EDDY SIMULATION OF RAMJET TO SCRAMJET TRANSITION Thommie Nilsson¹, Christer Fureby¹; ¹Lund University, Sweden | |||
06. Sep 22 | 11:30 | 12:00 | 9.1.3 |
AEROPROPULSIVE CHARACTERIZATION OF THE HYPERSONIC CRUISER VEHICLE IN STRATOFLY PROJECT P. Roncioni¹, L. Cutrone¹, M. Marini¹; ¹CIRA, Italy | |||
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06. Sep 22 | 10:30 | 11:00 | 10.1.1 |
ENVIRONMENTAL ASSESSMENT OF NOISE ABATEMENT APPROACH TRAJECTORIES E. M. Thoma¹, T. Grönstedt¹, E. Otero, KTH, Royal Institute of Technology, Sweden; X. Zhao¹; ¹Chalmers University of Technology, Sweden | |||
06. Sep 22 | 11:00 | 11:30 | 10.1.2 |
A MULTIPLE MODEL ADAPTIVE ESTIMATOR FOR AIRCRAFT AERODYNAMIC PARAMETER AND THRUST DEVIATION IDENTIFICATION D. Ding, China Aerodynamics Research and Development Center, China | |||
06. Sep 22 | 11:30 | 12:00 | 10.1.3 |
DESIGN OF A TYPICAL MANEUVERING PROCESS SIMULATION TEST CONTROL SYSTEM WITH CONTROLLABLE RUDDER SURFACE J.-F. Wang, China; H. Tan, China; H. Chen, China; S. Feng, China; M.-H. Wang, China | |||
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06. Sep 22 | 10:30 | 11:00 | 11.1.1 |
PREPARATORY RESEARCH FOR UAM COLLISION AVOIDANCE USING ADSB Seokmin Ahn¹, Hyunjin Choi¹, Sungyuk Kim¹, Jaeeun Kim¹, Hyeok Ryu¹; ¹Korea Aerospace Research Institute, South Korea | |||
06. Sep 22 | 11:00 | 11:30 | 11.1.2 |
SAFE REINFORCEMENT LEARNING BASED MULTIROTOR COLLISION AVOIDANCE WITH UNEXPECTED OBSTACLES H.J. Ahn¹, C.S. Lim¹, D.W. Lee¹, H.C. Bang¹; ¹Korea Advanced Institute of Science and Technology(KAIST), South Korea | |||
06. Sep 22 | 11:30 | 12:00 | 11.1.3 |
INVESTIGATION OF SIMULATION FRAMEWORKS FOR THE EVALUATION OF AUTOMATED FLIGHT FUNCTIONS FOR EVTOL AIRCRAFT Yves Lemmens¹, Casper Teirlink¹, Anoosh Hegde¹, David Pla Guerrero¹, Gerardo Olivares², Harsh Shah²; ¹Siemens Digital Industries Software, Belgium ;²National Institute for Aviation Research, United States | |||
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06. Sep 22 | 10:30 | 11:00 | 12.1.1 |
SMART SKIN FOR AEW AIRCRAFT Prabhat Khanal, Chalmers University of Technology, Sweden; Per Hallander¹, Ruoshan Luo¹; ¹Saab AB, Sweden | |||
06. Sep 22 | 11:00 | 11:30 | 12.1.2 |
CERTIFICATION ASPECTS OF AN EARTH OBSERVATION PAYLOAD INSTALLED ON COMMERCIAL TRANSPORT AIRCRAFT R. Lopez Pereira, Safran Engineering Services GmbH, Germany; L. Rammos, Skyflox Sarl, Luxembourg | |||
06. Sep 22 | 11:30 | 12:00 | 12.1.3 |
DESIGN OF ELECTRONICALLY PHASE-TUNING REFLECTARRAY ANTENNA FOR AIRBORNE RADAR APPLICATION Gexing Kong, China; Peng Cui, China; Wei Du, China; Rui Chen, China | |||
Reserve Paper | 12.1.R |
CALVERT AND PAPI LIGHT SYSTEM USED FOR AN AUTOMATIC APPROACH AND LANDING T. R. Rogalski, Rzeszow University of Technology,, Poland | |||||
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06. Sep 22 | 10:30 | 11:00 | 13.1.1 |
TECHNICAL CONCEPTS FOR INSPECTING UAVS FOR DAMAGE J. Eltgen¹, T. Schüppstuhl¹; ¹Hamburg University of Technology, Germany | |||
06. Sep 22 | 11:00 | 11:30 | 13.1.2 |
LOCALIZATION OF INTERROGATORS WITH A 1030/1090 MHZ SPECTRUM MONITORING SYSTEM Luciano Sarperi¹, Michael Jäger¹, Pascal Müller¹, Michael Felux¹; ¹ZHAW, Switzerland Presenter: Michael Jäger, ZHAW School of Engineering | |||
06. Sep 22 | 11:30 | 12:00 | 13.1.3 |
A FEDERATED LEARNING BASED SECURITY FOR CONTROLLER-PILOT DATA LINK COMMUNICATION Suleman Khan¹, Gurjot Singh Gaba¹, Andrei Gurtov¹; ¹Linköping University, Sweden Presenter: Suleman Khan, Linköping University |
12:00 - 13:00 | Lunch Break |
0.3 | ICAS Enoch Thulin Lecture for Innovation in Aeronautics“Reflections on Active Aeroelastic Control and the Multidisciplinary Design Optimization of Aircraft” Eli Livne Chair: C. Atkin ICAS PPSC Chair | |||
06. Sep 22 | 13:00 | 14:00 |
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06. Sep 22 | 14:00 | 14:30 | 1.2.1 |
DYNAMIC PAIRWISE WAKE VORTEX SEPARATIONS FOR ARRIVALS USING PREDICTIVE MACHINE LEARNING MODELS L Frigerio¹, I De Visscher, Wake Prediction Technologies (WaPT), Belgium; G Stempfel¹, R Barragan Montes², C Chalon Morgan²; ¹Euranova, Belgium ;²EUROCONTROL, Belgium Presenter: Lorenzo Frigerio, Euranova | |||
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06. Sep 22 | 14:00 | 14:30 | 2.2.1 |
MORE ELECTRIC AIRCRAFT (MEA) SCALING ASPECTS AND WEIGHT IMPACT E. Holmgren¹, D. Haldar¹, L. Bertling Tjernberg, School of Electrical Engineering and Computer Science, KTH Royal, Sweden; A. Johansson, SAAB, Sweden; ¹KTH Royal Institute of Technology, Sweden | |||
06. Sep 22 | 14:30 | 15:00 | 2.2.2 |
SIZING AND OPTIMIZATION OF A MORE ELECTRIC AIRCRAFT INTEGRATING SHORT-TERM INCREMENTAL TECHNOLOGIES T. Planès¹, S. Delbecq¹, V. Pommier-Budinger¹, V. Palanque¹, E. Bénard¹; ¹ISAE-SUPAERO, France | |||
06. Sep 22 | 15:00 | 15:30 | 2.2.3 |
IMPLEMENTATION OF WING ICE PROTECTION SYSTEM IN MORE ELECTRIC AIRCRAFT TECHNOLOGIES D. Haldar¹, E. Holmgren¹, A. Johansson¹; ¹KTH Royal Institute of Technology, Sweden | |||
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06. Sep 22 | 14:00 | 14:30 | 3.2.1 |
AEROSHAPE AND TRAJECTORY DESIGN OF NEXT GENERATION RE-ENTRY VEHICLES Montella Nicolina¹, Andrea Aprovitola¹, Luigi Iuspa¹, Giuseppe Pezzella¹; ¹University of Campania , Italy | |||
06. Sep 22 | 14:30 | 15:00 | 3.2.2 |
CONCEPT DESIGN OF A LOW BOOM SSBJ TO SATISFY SOCIAL ACCEPTABILITY Shigeru Horinouchi, SuperSonic Jet Planning Inc., Japan | |||
06. Sep 22 | 15:00 | 15:30 | 3.2.3 |
A RAPID DESIGN METHOD FOR QUIET SPIKE OF SUPERSONIC TRANSPORT AIRCRAFT L-W Zhang¹, Z-H Han¹, J-L Qiao¹, Y-L Ding¹, Q Chen¹, W-P Song¹; ¹Northwestern Polytechnical University, China | |||
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06. Sep 22 | 14:00 | 14:30 | 4.2.1 |
ADJOINT SENSITIVITY ANALYSIS OF TIME DEPENDENT FLOWS WITH RESPECT TO NON-GEOMETRICAL PARAMETERS T. S. Privato¹, J. S. B. Lima, IMT, Brazil; D. I. Dolci¹, M. T. Hayashy, UFABC, Brazil; B. S. Carmo¹, E. V. Volpe¹; ¹USP, Brazil Presenter: Ernani Volpe, USP | |||
06. Sep 22 | 14:30 | 15:00 | 4.2.2 |
POWER, COMPRESSION AND EFFICIENY: A BLADE PROFILE PARAMETRIC STUDY ON MULTI-STAGE AXIAL COMPRESSOR A Koksal, Turkey | |||
06. Sep 22 | 15:00 | 15:30 | 4.2.3 |
AUTOMATIC FREE-FORM DEFORMATION AS GEOMETRIC PARAMETERIZATION FOR AERDYNAMIC DESIGN Matunaga, M.A.L. Marco Aurélio Leonel Matunaga, ITA - Instituto Tecnológico de Aeronáutica, Brazil; Azevedo, J. L. F Joao Luiz Filgueiras de Azevedo, IAE - Instituto de Aeronáutica e Espaço, Brazil | |||
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06. Sep 22 | 14:00 | 14:30 | 5.2.1 |
STABILITY OF A LAMINAR BOUNDARY LAYER OVER A LOCALISED SURFACE INDENTATION E. R. Gowree, ISAE-SUPAERO, France; C. J. Atkin, University of East Anglia, United Kingdom | |||
06. Sep 22 | 14:30 | 15:00 | 5.2.2 |
DIRECT NUMERICAL SIMULATIONS OF A TURBULENT AIR INTAKE Y.-C. Xi, Tsinghua University, China | |||
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06. Sep 22 | 14:00 | 14:30 | 6.2.1 |
PRELIMINARY AERODYNAMIC WING DESIGN OPTIMISATION FOR WING-IN-GROUND EFFECT AIRCRAFT Rejish Jesudasan¹, Raffaello Mariani¹, Ardeshir Hanifi¹; ¹KTH Royal Institute of Technololgy, Stockholm, Sweden | |||
06. Sep 22 | 14:30 | 15:00 | 6.2.2 |
AERODYNAMIC ANALYSIS OF LOW SPEED TANDEM CHANNEL WING FOR EVTOL AIRCRAFT CONSIDERING PROPELLER-WING INTERACTION .M Chang¹, Z.Y. Zheng¹, X.X Meng¹, J.Q Bai¹, B. Wang, Chinese Academy of Sciences, China; ¹Northwestern Polytechnical University, China Presenter: Zhongyuan Zheng, Northwestern Polytechnical University | |||
06. Sep 22 | 15:00 | 15:30 | 6.2.3 |
ON THE APPLICABILITY ASSESSMENT OF VON KARMAN’S MOMENTUM THEORY IN PREDICTING THE WATER-ENTER LOAD OF V-SHAPED BODY Y. Lu, China; A. Del Buono, Italy; T. Xiao, China; A. Iafrati, Italy; J. Xu, China | |||
Reserve Paper | 6.2.R |
AERODYNAMIC AND AEROTHERMODYNAMIC ASSESSMENT OF A LIFTING-BODY RE-ENTRY VEHICLE Andrea Aprovitola¹, Nicolina Montella¹, Luigi Iuspa¹, Giuseppe Pezzella¹, Antonio Viviani¹; ¹University of Campania , Italy | |||||
Reserve Paper (interactive) | 6.2.R |
NUMERICAL STUDY ON WATER DISPLACEMENT DRAG CHARACTERISTICS OF AIRCRAFT ELASTIC TIRE ON CONTAMINATED RUNWAYS C. H. Ge¹, P. Q. Liu¹, Q. L. Qu¹; ¹Beihang University, China | |||||
Reserve Paper (interactive) | 6.2.R |
EFFICIENT MID-FIDELITY AERODYNAMIC MODELING OF A TILT-WING EVTOL FOR CONTROL APPLICATIONS D. Perdolt¹, D. Milz¹, M. May¹, M. Thiele, Technical University of Munich, Germany; ¹German Aerospace Center, Germany Presenter: Daniel Perdolt, German Aerospace Center Institute of System Dynamics and Control | |||||
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06. Sep 22 | 14:00 | 14:30 | 7.2.1 |
TI-6AL-4V ADDITIVE MANUFACTURING MEASURE OF QUALITY ACCORDING TO FATIGUE CRACK INITIATION VS. CRACK PROPAGATION C. Matias¹, A. Diskin¹, O. Golan, Afeka- Tel-Aviv Academic College of Engineering, Israel; A. Garkun², E. Strokin²; ¹Israel Aerospace Industries (IAI), Israel ;²The Israel Institute of Metals,, Israel | |||
06. Sep 22 | 14:30 | 15:00 | 7.2.2 |
DEFECT BASED MODELLING OF LIFE IN ELECTRON BEAM MELTED TI-6AL-4V H. Sandell, Luleå University of Technology, Sweden | |||
06. Sep 22 | 15:00 | 15:30 | 7.2.3 |
RVE-BASED HOMOGENIZATION OF ADDITIVELY MANUFACTURED POROUS METALS A. Alaimo¹, G. Mantegna¹, C. Orlando¹, D. Tumino¹, C. Vindigni¹; ¹Faculty of Engineering and Architecture Kore University of Enna, Italy | |||
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06. Sep 22 | 13:30 | 14:00 | 8.2.1 |
DESIGN AND EXPERIMENTAL TESTING OF A DROOP NOSE MORPHING FOR ADVANCED REGIONAL AIRCRAFT A. De Gaspari¹, V. Cavalieri¹, S. Ricci¹; ¹Politecnico di Milano, Italy | |||
06. Sep 22 | 14:00 | 14:30 | 8.2.2 |
STRUCTURAL ANALYSIS OF TWISTED/CURVED BEAMS USING A HYBRID METHOD A. Siami¹, F. Nitzsche¹; ¹Carleton University, Canada Presenter: Fred Nitzsche, Carleton University | |||
06. Sep 22 | 15:00 | 15:30 | 8.2.3 |
EXPERIMENTAL AND NUMERICAL ANALYSES OF A PRE-STRESSED TENSEGRITY MEMBRANE V. A. S. Paiva¹, L. H. S. Teixeira¹, J. H. Izuka¹, P. G. Ramos¹, P. R. G. Kurka¹; ¹UNICAMP, Brazil | |||
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06. Sep 22 | 14:00 | 14:30 | 9.2.1 |
MULTI-PLATFORM APP-EMBEDDED MODEL FOR HYBRID AIR-BREATHING ROCKET-CYCLE ENGINE IN HYPERSONIC ATMOSPHERIC ASCENT S. Tsentis, Greece Presenter: Spyros Tsentis, Aristotle University of Thessaloniki | |||
06. Sep 22 | 14:30 | 15:00 | 9.2.2 |
SAND EROSION MODELING IN GENERIC COMPRESSOR RIG TESTING Xija wu¹, Qi Yang¹; ¹National Research Council Canada, Canada | |||
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06. Sep 22 | 14:00 | 14:30 | 10.2.1 |
HANDLING QUALITIES OF A DISTRIBUTED PROPULSION ELECTRIC AIRCRAFT D PLANAS ANDRES, ONERA & ISAE SUPAERO, France; C DOLL, ONERA, France; P PASTOR, ISAE SUPAERO, France | |||
06. Sep 22 | 14:30 | 15:00 | 10.2.2 |
PRELIMINARY STUDY ON A DESIGN OF A RETURN FLIGHT TRAJECTORY OF A SUBORBITAL VEHICLE A. Kwiek¹, M. Figat¹, T. Goetzendorf-Grabowski ¹; ¹Warsaw University of Technology, Poland | |||
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06. Sep 22 | 13:30 | 14:00 | 11.2.1 |
NUMERICAL MODELLING OF PITCHING WINGS FOR GUST MITIGATION Weixing Yuan¹, Alanna Wall¹, Xiaoyang Zhang², Dominique Poirel²; ¹National Research Council (NRC) Canada, Canada ;²Royal Military College of Canada (RMC),, Canada | |||
06. Sep 22 | 14:00 | 14:30 | 11.2.2 |
UNMANNED AERIAL VEHICLE\\\\\\\'S TRAJECTORY OPTIMIZATION IN CONSTRAINED ENVIRONMENTS J. Novák ¹, P. Chudý¹; ¹Brno University of Technology, Czech Republic | |||
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06. Sep 22 | 14:00 | 14:30 | 12.2.1 |
MACHINE LEARNING IN SHIP MOTION PREDICTION AND UAV RECOVERY J Lakkis¹, B Cees¹; ¹RMIT University, Australia | |||
06. Sep 22 | 14:30 | 15:00 | 12.2.2 |
AIRCRAFT FUEL LEVEL GAUGE MECHANISMS: A HIGH PRECISION FUEL SYSTEM IN ACROBAT-CRAFTS M. A. D. Di Marzo, University of São Paulo, Brazil | |||
06. Sep 22 | 15:00 | 15:30 | 12.2.3 |
VISION-BASED LOCALISATION FOR AUTONOMOUS AERIAL NAVIGATION IN GNSS-DENIED SITUATIONS D. Sabel¹, A. Maki¹, T. Westin², D. Åsvärn²; ¹KTH Royal Institute of Technology, Sweden ;²Spacemetric AB, Sweden | |||
Reserve Paper | 12.2.R |
INNOONBOARD FOR IMPROVED IMAGE HANDLING IN AIRBORNE COASTAL RECONNAISSANCE – A PROJECT PRESENTATION D. Åkerman¹, O. Fästh, ST Airborne Solutions, Sweden; M. Persson, Unibap, Sweden; D. Sabel¹, D. Åsvärn¹; ¹Spacemetric, Sweden Presenter: Daniel Sabel, Spacemetric | |||||
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06. Sep 22 | 14:00 | 14:30 | 13.2.1 |
MANUFACTURE OF LARGE-SCALE SPACE EXPLORATION COMPONENTS USING WIRE + ARC ADDITIVE MANUFACTURING C Diao¹, E Eimer¹, S Mancini, Thales Alenia Space, Italy; S Krishnaswamy¹, F Schwarz¹, E Pagone¹, J Ding¹, S Williams¹, Z Pinter², F Martina²; ¹Cranfield University, United Kingdom ;²WAAM3D, United Kingdom | |||
06. Sep 22 | 14:30 | 15:00 | 13.2.2 |
LATEST DEVELOPMENTS IN HIGH PRESSURE HEAT TREATMENT OF AEROSPACE COMPONENTS Chad Beamer, Quintus Technologyes LLC, United States; Anders Magnusson, Quintus Technologies AB, Sweden | |||
06. Sep 22 | 15:00 | 15:30 | 13.2.3 |
VIKA-CONCEPT OF A DIGITAL PLATFORM FOR IMPLICIT KNOWLEDGE AND VIRTUAL ASSISTANCE FOR ADDITIVE MANUFACTURED PARTS J. Steffen, HAW Hamburg, Germany | |||
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06. Sep 22 | 14:00 | 14:30 | 14.2.1 |
A FRAMEWORK FOR INNOVATION WITHIN AEROSPACE SEGMENT C Jochims Lau¹, A. G. Slongo¹, T. V. Bins¹, G. L. de Oliveirra¹; ¹AEL Sistemas, Brazil | |||
06. Sep 22 | 14:30 | 15:00 | 14.2.2 |
INTEGRATE ONLINE QUERY&DEFENSE INTO PROJECT BASED LEARNING TO PROMPT ENGINEERING AUTHENTIC EXPERIENCES S. Sun, Civil Aviation University of China, China; R. Gong, University of Waterloo, Canada Presenter: shuguang SUN, Civil Aviation University of China |
15:30 - 16:00 | Break |
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06. Sep 22 | 16:00 | 16:30 | 1.3.1 |
NATO AVT-297 DEVELOPMENT OF A FRAMEWORK FOR VALIDATION OF COMPUTATIONAL TOOLS FOR ANALYSIS OF AIR VEHICLES J. Morrison¹, M. Nikbay, Istanbul Technical University, Turkey; E. Walker¹; ¹NASA Langley Research Center, United States | |||
06. Sep 22 | 16:30 | 17:00 | 1.3.2 |
A MODEL VALIDATION HIERARCHY FOR CONNECTING SYSTEM DESIGN TO MODELING AND SIMULATION CAPABILITIES J.M. Luckring, NASA Langley Research Center, United States; S. Shaw, MBDA UK Ltd., United Kingdom; W.L. Oberkampf, WLO Consulting, Inc., United States; R. Graves, Air Force Research Laboratory, United States | |||
06. Sep 22 | 17:00 | 17:30 | 1.3.3 |
SYSTEM LEVEL IDENTIFICATION OF CRITICAL UNCERTAINTIES TO ENABLE VALIDATION EXPERIMENTS D. Mavris¹, E.Y. Yarbasi¹, B. Bagdatli¹; ¹Georgia Institute of Technology, United States | |||
06. Sep 22 | 17:30 | 18:00 | 1.3.4 |
OPEN PANEL DISCUSSION op panel, United States | |||
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06. Sep 22 | 16:00 | 16:30 | 2.3.1 |
BOEING/SAAB CO-DEVELOPMENT PROGRAMME OF T-7A TRAINER - A JOINT DIGITAL JOURNEY (invited) Donn C. Yates, Boeing, United States Presenter: Tomas Karlsson, Saab | |||
06. Sep 22 | 16:30 | 17:00 | 2.3.2 |
TOWARDS A SEAMLESS SIMULATION OF THE AIR TRANSPORT SYSTEM E. Moerland¹, A. Mancini¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany | |||
06. Sep 22 | 17:00 | 17:30 | 2.3.3 |
DIGITAL COLLABORATIVE DESIGN: AN INNOVATIVE FRAMEWORK IN AERONAUTICAL EDUCATION Z Cui¹, M Luo¹, H Liu¹, X Sun¹, Z Ji¹, Y Hua, China Academy of Launch Vehicle Technology, China; ¹Beihang University, China | |||
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06. Sep 22 | 16:00 | 16:30 | 3.3.1 |
INNOVATIVE URBAN AIR MOBILITY FROM THE PERSPECTIVE OF THE HAMBURG METROPOLITAN REGION Daniel Kloock-Schreiber¹, Majed Swaid², Volker Gollnick¹, Alexander Fay, HSU, Institute of Automation Technology, Germany; Malte Niklaß²; ¹TUHH, Institute of Air Transportation Systems, Germany ;²DLR, Institute of Air Transportation Systems, Germany | |||
06. Sep 22 | 16:30 | 17:00 | 3.3.2 |
ESTIMATION OF EVTOL FLIGHT PERFORMANCE USING ROTORCRAFT THEORY Y. Fukumine¹, Z. LEI¹; ¹Suwa University of Science, Japan | |||
06. Sep 22 | 17:00 | 17:30 | 3.3.3 |
COMPUTATIONAL INVESTIGATION ON AERODYNAMIC CHARACTERISTICS OF COAXIAL ROTORS FOR EVTOL AIRCRAFT Z. Xu, Northwestern Polytechnical University, China; M. Chang¹, J. Bai¹, M. Dai, China North Industries Corporation (NORINCO), Germany; ¹Unmanned System Research Institute, Northwestern Polytechnical, China | |||
06. Sep 22 | 17:30 | 18:00 | 3.3.4 |
MIXED INTEGER NONLINEAR PROGRAMMING FOR EVTOL AIRCRAFT DESIGN AND OPTIMIZATION Tianhong Jiang¹, Mingkang Li¹, Yaolong Liu¹, Yao Zheng¹; ¹School of Aeronautics and Astronautics, Zhejiang University, China Presenter: Tianhong Jiang | |||
Reserve Paper | 3.3.R |
RESEARCH ON THE DESIGN OF UNMANNED AERIAL VERICLE FOR MINE INSPECTION Zhan-Ke Li¹, Shi-Gao Su, Aerospace Times Feihong Technology Co., Ltd. , China; Zhi-Yu Li¹, Fu-Rong Li¹, Gao Chao¹; ¹Northwestern Polytechnical University, China Presenter: Zhi-Yu Li, Northwestern Polytechnical University | |||||
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06. Sep 22 | 16:00 | 16:30 | 4.3.1 |
EFFECT OF LES LENGTH SCALE AND NUMERICAL SCHEME IN HYBRID RANS-LES OF FREE SHEAR LAYER FLOWS S. Arvidson¹, M. Carlsson, Chalmers University of Technology, Sweden; S. Nilsson¹; ¹Saab Aeronautics, Sweden | |||
06. Sep 22 | 16:30 | 17:00 | 4.3.2 |
INVESTIGATION OF LEADING-EDGE VORTICES ON A TRIPLE-DELTA-WING CONFIGURATION USING SCALE-ADAPTIVE SIMULATION Tony Di Fabbio¹, Eike Tangermann¹, Markus Klein¹; ¹Universität der Bundeswehr München, Germany | |||
06. Sep 22 | 17:00 | 17:30 | 4.3.3 |
NUMERICAL INVESTIGATION OF HYPERSONIC TURBULENT BOUNDARY LAYERS WITH HIGH-TEMPERATURE EFFECTS D. Passiatore¹, L. Sciacovelli, ENSAM Paris, France; P. Cinnela , Sorbonne Université, France; G. Pascazio¹; ¹Politecnico di Bari, Italy | |||
06. Sep 22 | 17:30 | 18:00 | 4.3.4 |
HYBRID RANS-LES MODELLING: SOME RECENT DEVELOPMENT AND AERODYNAMIC APPLICATIONS S.-H. Peng, Swedish Defence Research Agency, FOI, Sweden Presenter: Shia-Hui Peng, Swedish Defence Research Agency, FOI | |||
Reserve Paper | 4.3.R |
HEAT TRANSFER MODULATION BY SUSPENDED PARTICLES IN A SHEARLESS MIXING LAYER Hamid Reza Zandi Pour¹, Michele Iovieno¹; ¹Politecnico di Torino, Italy | |||||
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06. Sep 22 | 16:00 | 16:30 | 5.3.1 |
ANALYSIS OF THE STABILITY OF MULTIPLE HELICAL VORTICES USING COMPLEX-STEP LINEARIZATION V. G. Kleine, ITA, Brazil; A Hanifi¹, D. S. Henningson¹; ¹KTH, Sweden | |||
06. Sep 22 | 16:30 | 17:00 | 5.3.2 |
EXPERIMENTAL EVALUATION OF A PASSIVE FLOW-CONTROL DEVICE FOR A TILT-ROTOR AIRCRAFT A R Proenca¹, S P Prince¹, Lynton Banks-Davies¹, K P Garry¹; ¹Cranfield University, United Kingdom | |||
06. Sep 22 | 17:00 | 17:30 | 5.3.3 |
STUDY ON FLOW AND HEAT TRANSFER CHARACTERISTICS OF SUPERCRITICAL RP-3 KEROSENE IN AN INCLINED RECTANGULAR CHANNEL J.-J. Yu, Chonqqing University, China | |||
06. Sep 22 | 17:30 | 18:00 | 5.3.4 |
RESEARCH ON PRESSURE LOAD OF AN EMBEDDED JET NOZZLE Hongyang Li¹, Xiao Wang¹, Dongsheng Yu¹, Fangliang Liu¹; ¹Shenyang Aircraft Design and Research Institute, China | |||
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06. Sep 22 | 16:00 | 16:30 | 6.3.1 |
WIND TUNNEL TESTS RESULTS AND PERFORMANCE OF THE MOTHIF BLOWN FLAP P. D'Alesio¹, G. Travostino¹, P. Planquart², G. Glabeke²; ¹Piaggio Aerospace, Italy ;²von Karman Institute, Belgium | |||
06. Sep 22 | 16:30 | 17:00 | 6.3.2 |
A STUDY OF HIGH-LIFT DEVICES FOR LOW REYNOLDS NUMBER APPLICATIONS Y. Leng¹, K. Fayez, DELAIR, France; J.-M. Moschetta¹, M. Bronz, ENAC, France; ¹ISAE-SUPAÉRO, France | |||
06. Sep 22 | 17:00 | 17:30 | 6.3.3 |
COMPLETION OF AN EXISTING FAST TURN-AROUND SLAT NOISE PREDICTION MODEL BASED ON STATISTICAL ANALYSIS Jose Manuel Rendón-Arredondo¹, Laura Botero-Bolívar², Alejandro Marulanda-Tobon¹, Henry Laniado¹, Leandro de Santana²; ¹Universidad EAFIT, Colombia ;²University of Twente, Netherlands | |||
06. Sep 22 | 17:30 | 18:00 | 6.3.4 |
MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION OF 2D HIGH-LIFT DEVICE BASED ON DISTRIBUTED DEEP REINFORCEMENT LEARNING J.-H. Dai¹, P.-Q. Liu¹, L. Li¹; ¹Beihang University, China | |||
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06. Sep 22 | 16:00 | 16:30 | 7.3.1 |
WING STATIC STRUCTURAL ANALYSIS AND EXPERIMENTAL TESTING OF A COMPOSITE 1:8 S55-X REPLICA G Nicolosi¹, A Lunghitano ¹, S Lombardi ¹, T Talamucci¹, A Caivano¹, N Simone¹, E Cestino¹, V Sapienza, Aeronautical Engineering Consultant, Italy; ¹Politecnico di Torino, Italy | |||
06. Sep 22 | 16:30 | 17:00 | 7.3.2 |
ASSESSMENT OF FAILURE UNDER LONGITUDINAL COMPRESSION OF UNIDIRECTIONAL COMPOSITES WITH IN-PLANE FIBER MISALIGNMENT A.R. de Faria, ITA, Brazil Presenter: Alfredo Rocha de Faria, ITA | |||
06. Sep 22 | 17:00 | 17:30 | 7.3.3 |
DAMAGE QUANTIFICATION ON COMPOSITE STRUCTURES UTILIZING NEURAL NETWORKS AND HYBRID DATA L. P. S. Ferreira¹, M. O. Yano², S. Silva², C. A. Cimini¹; ¹UFMG, Brazil ;²UNESP, Brazil | |||
06. Sep 22 | 17:30 | 18:00 | 7.3.4 |
TRIBOLOGICAL AND STRUCTURAL EVALUATION OF 3D EPOXY RESINS G.C Cristea¹, A. Stefan¹, K.K Krawczyk, Joanneum Research, Austria; C.-E Pelin¹, S. Ilina¹; ¹INCAS, Romania | |||
Reserve Paper | 7.3.R |
DOPAMINE COATED UHMWPE HYDROGEN-RICH / BENZOXAZINE COMPOSITES FOR SPACE RADIATION SHIELDING J.H Cha¹, C.G Kim¹; ¹KAIST, South Korea | |||||
Reserve Paper (interactive) | 7.3.R |
STUDY ON MECHANICAL PROPERTIES OF CARBON FIBER RESIN MATRIX COMPOSITE BOLTED JOINT STRUCTURE AT HIGH TEMPERATURE D. WANG, School of Aeronautics, Northwestern Polytechnical University, Xi, China; G.W. LI, School of civil aviation, Northwestern Polytechnical University, China; H.Y. HUANG, School of Aeronautics, Northwestern Polytechnical University, China Presenter: Dong Wang, Northwestern Polytechnical University | |||||
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06. Sep 22 | 16:00 | 16:30 | 8.3.1 |
AEROELASTIC MODELING, LOADS ANALYSIS AND STRUCTURAL DESIGN OF A FIGHTER AIRCRAFT A. Voß¹, T. Klimmek¹; ¹DLR Institute of Aeroelasticity , Germany | |||
06. Sep 22 | 16:30 | 17:00 | 8.3.2 |
LOADS ANALYSIS AND STRUCTURAL OPTIMIZATION OF A LONG-RANGE TRANSPORT CONFIGURATION WITH HYBRID LAMINAR FLOW CONTROL V. Handojo¹, T. Klimmek¹, T. Streit, DLR - Institute of Aerodynamics and Flow Technology, Germany; ¹DLR - Institute of Aeroelasticity, Germany | |||
06. Sep 22 | 17:00 | 17:30 | 8.3.3 |
TRANSIENT RELEASE AND LATERAL GUST BEHAVIOUR OF AIRCRAFT INCORPORATING THE SEMI AEROELASTIC HINGE R.C.M, Cheung¹, H. Gu¹, F. Healy¹, D. Rezgui¹, J.E. Cooper¹; ¹University of Bristol, United Kingdom | |||
06. Sep 22 | 17:30 | 18:00 | 8.3.4 |
SET-BASED DESIGN COORDINATION BETWEEN COUPLE SYSTEMS: A WING AERO-STRUCTURAL DESIGN PERSPECTIVE X. Chen¹, A. Riaz¹, M. D. Guenov¹; ¹Cranfield University, United Kingdom | |||
Reserve Paper (interactive) | 8.3.R |
DEVELOPMENT OF NOVEL ANALYTICAL METHOD FOR TIME DOMAIN AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO WING USING UNSTEADY IND Zia Ur Rehman Rehman, Pakistan | |||||
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06. Sep 22 | 16:00 | 16:30 | 9.3.1 |
LATTICE BOLTZMANN METHOD FOR BROADBAND NOISE PREDICTIONS ON A TURBULENCE-CASCADE TEST RIG INCLUDING SERRATED VANES M. Buszyk¹, L. Vienne², T. Le Garrec¹, J.-F. Boussuge², C. Polacsek¹, R. Barrier¹; ¹ONERA, France ;²CERFACS, France | |||
06. Sep 22 | 16:30 | 17:00 | 9.3.2 |
OPTIMIZATION OF INSTALLED COMPACT AND ROBUST NACELLES USING SURROGATE MODELS F. Sánchez-Moreno¹, D. MacManus¹, J. Hueso-Rebassa¹, F. Tejero¹, C. Sheaf, Rolls Royce, United Kingdom; ¹Cranfield University, United Kingdom | |||
06. Sep 22 | 17:00 | 17:30 | 9.3.3 |
AEROACOUSTIC PERFORMANCES OF A LOW-NOISE AIRFOIL CASCADE WITH SERRATED LEADING EDGES: PREDICTIONS AND MEASUREMENTS C. POLACSEK¹, M. BUSZYK¹, R. BARRIER¹, V. CLAIR², E. SALZE²; ¹ONERA, France ;²LMFA, France | |||
06. Sep 22 | 17:30 | 18:00 | 9.3.4 |
EFFECT OF HEAT EXCHANGER INTEGRATION IN AERODYNAMIC OPTIMISATION OF AN AGGRESSIVE S-DUCT Isak Jonsson¹, Robert Ranman¹, Xisto Carlos ¹, Tomas Grönstedt¹; ¹Chalmers Tekniska Hogskola AB, Sweden | |||
Reserve Paper | 9.3.R |
MULTIPOINT AERODYNAMIC DESIGN OF A SHORT NACELLE FOR AN ELECTRIC FAN V. T Silva¹, M. Lejon ², A. Lundbladh², C. Xisto¹, A. Venkatesh ¹; ¹Chalmers University of Technology, Sweden ;²GKN Aerospace, Sweden | |||||
Reserve Paper | 9.3.R |
EFFECT OF TAILCONE SHAPE ON HOT STREAK PHENOMENA AND INFRARED SIGNATURE OF SERPENTINE NOZZLE WITH AFT DECK J.-Z. Fan¹, Q.-Z. Yang¹, X.-B. Du¹, H.-Q. Yang¹, Y.-B. He¹, Y.-Q. Shi¹; ¹Northwestern Polytechnical University, China | |||||
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06. Sep 22 | 16:00 | 16:30 | 10.3.1 |
AUTOMATIC TAKE-OFF AND LANDING OF A VERY LIGHT ALL ELECTRIC OPTIONALLY PILOTED AIRCRAFT S.P. Scherer¹, M. Speckmaier¹, D. Gierszewski¹, C. Mishra¹, A. Steinert¹, R. Steffensen¹, S. Wulf¹, F. Holzapfel¹; ¹Technical University of Munich,, Germany | |||
06. Sep 22 | 16:30 | 17:00 | 10.3.2 |
LPV/LFR CONTROL FOR ACTIVE FLUTTER SUPPRESSION OF A SMART AIRFOIL MODEL Renan Pereira, ITA, Brazil; Pedro González¹, Flávio Silvestre¹; ¹TU Berlin, Germany | |||
06. Sep 22 | 17:00 | 17:30 | 10.3.3 |
LQR BASED DIGITAL AUTOPILOT FOR LIGHT SPORT AIRCRAFT Jan Vlk¹, Peter Chudy¹, Milan Prustomersky¹; ¹Brno University of Technology, Czech Republic | |||
06. Sep 22 | 17:30 | 18:00 | 10.3.4 |
EXTENSION OF THE CAPABILITIES OF AN AUTOMATIC LANDING SYSTEM WITH PROCEDURES MOTIVATED BY VISUAL-FLIGHT-RULES S.P. Scherer¹, C. Mishra¹, F. Holzapfel¹; ¹Technical University of Munich, Germany | |||
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06. Sep 22 | 16:00 | 16:30 | 11.3.1 |
FAULT DIAGNOSIS FOR SENSOR AND ACTUATOR OF HEXACOPTER UAV USING DUAL EXTENDED KALMAN FILTER Y.J. Kim¹, T.G. Kim¹, S.K. Kim¹; ¹Chungnam National University, South Korea | |||
06. Sep 22 | 16:30 | 17:00 | 11.3.2 |
CONTROL AUGMENTATION SYSTEM DESIGN FOR THE QUAD TILT-WING UAV VIA H-INFINITY STRUCTURE WITH GWO Kranthi Kumar Deveerasetty¹, Koichi OKA¹, Akinori HARADA¹; ¹Kochi University of Technology, Japan | |||
06. Sep 22 | 17:00 | 17:30 | 11.3.3 |
OPTIMIZATION OF ENERGY CONSUMPTION IN THE TRANSITION STATE OF A QUAD-PLANE T. Goetzendorf-Grabowski¹, D. Kacik¹, K. Pobikrowska, Lukasiewicz Research Network – Institute of Aviation, Poland; J. Mieloszyk¹; ¹Warsaw University of Technology, Poland | |||
06. Sep 22 | 17:30 | 18:00 | 11.3.4 |
FLIGHT VERIFICATION OF AUTOMATIC TRANSITION FOR QUAD TILT WING SMALL UAV Koji Muraoka¹, Masayuki Sato¹; ¹Japan Aerospace Exploration Agency, Japan | |||
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06. Sep 22 | 16:00 | 16:30 | 12.3.1 |
ELECTRICALLY POWERED LANDING GEAR SYSTEM FOR TRANSPORT AIRCRAFT TAXIING Ilan Berlowitz, IBAero Engineering, Israel | |||
06. Sep 22 | 16:30 | 17:00 | 12.3.2 |
AN INTEGRATED CONTROL SCHEME FOR STARTER/GENERATOR SYSTEM IN MORE ELECTRIC AIRCRAFT Hong Li, China; Zhengda Zhao, China; Zaihong Wan, China; Long Xu, China; Shuangxin Zhao, China; Pengyu Sun, China | |||
06. Sep 22 | 17:00 | 17:30 | 12.3.3 |
THE INFLUENCE OF THE MODEL PARAMETERS OF LIION BATTERIES ON THE WIRING HARNESS PERFORMANCE OF EVTOL AIRCRAFT S. Oberschwendtner¹, M. Hornung¹; ¹Technical University of Munich, Germany | |||
06. Sep 22 | 17:30 | 18:00 | 12.3.4 |
ANALYSIS AND DEVELOPMENT OF INTEGRATED LOW-PRESSURE SHAFT GENERATOR Magnus Genrup, Lund University, Sweden; Richard Avellán¹, Hans Mårtensson¹; ¹GKN Aerospace, Sweden | |||
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06. Sep 22 | 16:00 | 16:30 | 13.3.1 |
STUDY OF THE COST EFFICIENCY AND LAMINATE QUALITY USING DIFFERENT MOULD-MAKING TECHNOLOGIES L Loiodice¹, S Grendene¹, T Binetti¹, I Boni ¹, F Lovero ¹, R Piani¹; ¹Politecnico di Torino, Italy | |||
06. Sep 22 | 16:30 | 17:00 | 13.3.2 |
A VALUE-DRIVEN QUANTITATIVE FRAMEWORK CONCURRENTLY COUPLING AIRCRAFT DESING, MANUFACTURING AND SUPPLY CHAIN Giuseppa Donelli¹, João Mello², Felipe Odaguil², Thierry Lefebvre³, Nathalie Bartoli³, Ton van der Laan, GKN Fokker, Netherlands; Luca Boggero¹, Björn Nagel¹; ¹DLR, Germany ;²Embraer, Brazil ;³ONERA, France | |||
06. Sep 22 | 17:00 | 17:30 | 13.3.3 |
CONTRASTING YOLOV5 AND A CNN MODEL IN IDENTIFYING USER ACTION IN COMPUTER-AIDED MANUFACTURING IN REAL-TIME B. W. Peukert¹, J. Vesterberg¹, J. Birberg, Saab AB , Sweden; ¹KTH, Sweden Presenter: Bernd Walter Peukert, KTH | |||
06. Sep 22 | 17:30 | 18:00 | 13.3.4 |
DOMAIN MODEL CONSTRUCTION METHOD OF AVIATION EQUIPMENT MANUFACTURING OPERATION MANAGEMENT Chen Lin¹, Li Xiaohua¹, Zhang Zhengxin¹, Huang Wei¹, Wu RenZhong¹, Li Yan¹; ¹AVIC Chengdu Aircraft Industrial (Group) Co., Ltd., China | |||
Reserve Paper | 13.3.R |
RESEARCH ON COMMUNICATION AND DATA ACQUISITION TECHNOLOGY OF AVIATION SPECIAL EQUIPMENT LH.-Z. Zhong, Chengdu Aircraft Company, China | |||||
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06. Sep 22 | 16:00 | 16:30 | 14.3.1 |
INTEGRATED INTEGRATED SUAS TRAJECTORY OPTIMIZATION FOR DISASTER RESPONSE RECONNAISSANCE MISSIONS A. Andreeva-Mori¹, J. Homola², M. Johnson², K. Kobayashi¹, Y. Okuno¹, P. Kopardekar²; ¹JAXA, Japan ;²NASA, United States | |||
06. Sep 22 | 16:30 | 17:00 | 14.3.2 |
OVERVIEW OF JAXA AND NASA COLLABORATION ON MANNED AND UNMANNED AIRCRAFT OPERATION INTEGRATION IN DISASTER RESPONSE A. Andreeva-Mori¹, J. Homola², M. Johnson², K. Kobayashi¹, Y. Okuno¹, P. Kopardekar²; ¹JAXA, Japan ;²NASA, United States Presenter: Marcus Johnson, NASA | |||
06. Sep 22 | 17:00 | 17:30 | 14.3.3 |
DLR DESIGN CHALLENGE 2022 ON ADVANCED AERIAL FIREFIGHTING SYSTEMS OF SYSTEMS T. Dietl¹, P. Ratei¹, P. Shiva Prakasha¹, T. Zill¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany | |||
06. Sep 22 | 17:30 | 18:00 | 14.3.4 |
DESIGNING FOR SECURITY: A CYBERSECURITY INTRODUCTION FOR AEROSPACE EDUCATION K. Roush, United States |
18:00 - 19:30 | ICAS Speed Mentoring: For all early careers (students and young professionals) Meeting professionals from companies, research institutes, and universities in aeronautics all over the world |