33th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Session List

Please use your browser's search function (Ctrl+F) to look up a specific author or title.

Attention: Be advised that there might be changes till the congress, so please do not adjust your travel plans based on this preliminary programme.

"(invited)" behind a session means that those presentation were invited by the programme committee. They can, of course, be attended by everyone without "invitation

Monday, 05. Sep 2022

07:00 - 08:00Registration

08:00 - 09:00Opening Ceremony

0.1ICAS 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

10:00 - 10:30Coffee Break

1.1Sustainable Aircraft 1 (invited)
Chair(s): Mavris, D.
A1
15 - Guest lectures
05. Sep 22 10:30 11:00 1.1.1 FLYZERO: THE UK VISION FOR ZERO-CARBON EMISSION AIR TRAVEL (invited)
S. Pendry, ATI, United Kingdom
05. Sep 22 11:00 11:30 1.1.2 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
2.1MDAO 1
Chair(s): Bagassi, S.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
05. Sep 22 10:30 11:00 2.1.1 LARGE-SCALE MULTIFIDELITY AEROSTRUCTURAL OPTIMIZATION OF A TRANSPORT AIRCRAFT
N. 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
3.1Unconventional Configurations 1
Chair(s): Melkert, J.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
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
X. Zhao¹, C. Xisto¹, S.-H. Peng, Chalmers University of Technology/FOI, Sweden; ¹Chalmers University of Technology, Sweden
Reserve Paper 3.1.R EXPERIMENTAL INVESTIGATION OF A NEXT-GENERATION AIRLINER WITH BOUNDARY LAYER INGESTION
P.D. Bravo-Mosquera¹, J.P. Eguea¹, H.D. Cerón-Muñoz¹, F.M. Catalano¹; ¹University of São Paulo, Brazil
4.1Numerical Methods
Chair(s): , , Azevedo, J.L.F.
C 1
03.1 - Aerodynamics – CFD Methods and Validation
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
K. Sugaya¹, T. 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
K. Abe¹, S. Miyazaki¹, D. Sasaki¹, S. Takahashi², G. 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
5.1GARTEUR 1 (invited)
Chair(s): Tormalm, M.
C 2
15 - Guest lectures
05. Sep 22 10:30 11:00 5.1.1 GARTEUR: NEARLY HALF A CENTURY OF EUROPEAN COLLABORATION IN AERONAUTICS
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
G. Mingione, CIRA, Italy; P. Coustols, ONERA, France; F. Monge, INTA, Spain; H. van der Ven, NLR, Netherlands; K. Richter, DLR, Germany; M. Tormalm, FOI, Sweden; L.R. Calavera¹, B. Stefes¹, D. Pagan, MBDA, France; P. Eliasson, SAAB, Sweden; M. Mallet, DASSAULT, France; R. Gemma, LEONARDO, Italy; ¹AIRUBS, Spain
05. Sep 22 11:30 12:00 5.1.3 THE GROUP OF RESPONSABLES \"STRUCTURES AND MATERIALS (GOR SM)\": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES
H.G.S.J. Thuis, NLR, Netherlands
6.1Experimental Investigations on Laminar Flow
Chair(s): Hanifi, A.
C 3
03.2 - Experimental Aerodynamics
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 STABILTY AND TRANSITION OF A LAMINAR SEPARATION BUBBLE SUBJECTED TO FREESTREAM TURBULENCE
T. Jaroslawski¹, O. Vermeersch¹, J.-M. Moschetta², M. Forte¹, E. 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. Scarano¹, M.C. Jacob, Université de Lyon, France; X. Carbonneau¹, E.R. Gowree¹; ¹ISAE - SUPAERO, France
7.1Related Topics in Aircraft Design 1
Chair(s): Rinoie, K.
Bar 5
01.1 - Aircraft Design and Integrated System (Basics and Theory)
05. Sep 22 10:30 11:00 7.1.1 METHODOLOGIES AND EXAMPLE OF CONCEPTUAL DESIGN FOR A FOOT-LAUNCHABLE SPORT SAILPLANE
L.M.F. Barbosa, Heart Aerospace, Sweden
05. Sep 22 11:00 11:30 7.1.2 AIRFOIL DESIGN BY MULTI-ADDITIONAL SAMPLING MULTI-FIDELITY EFFICIENT GLOBAL OPTIMIZATION
K. Khankwa¹, T. Phiboon¹, A. Ariyarit¹, R. Kasemsri¹, M. Kanazaki, Tokyo Metropolitan University, Japan; ¹Suranaree University of Technology, Thailand
05. Sep 22 11:30 12:00 7.1.3 STRUCTURAL DESIGN AND FLUTTER ANALYSIS OF SWEPT BAFFLED INFLATABLE WING
N. Ma¹, F.-M. Meng¹, J.-H. Meng¹, L. Liu¹; ¹Beijing Institute of Technology, China
8.1Impact
Chair(s): Juracka, J., Ikeda, T.
23
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
05. Sep 22 10:30 11:00 8.1.1 A REDUCED ORDER MODEL FOR FULL-SCALE DRONE COLLISIONS
F. Franke¹, U. Burger¹, C. Hühne, German Aerospace Center, Germany; ¹Technische Hochschule Ingolstadt, Germany
05. Sep 22 11:00 11:30 8.1.2 HIGH FIDELITY AIRWORTHINESS BIRD AND DRONE STRIKE 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
05. Sep 22 11:30 12:00 8.1.3 XRF1 HIGH LIFT LOAD ANALYSIS OF WING AND HIGH LIFT SYSTEM
S. Pülm¹, V. Handojo¹, R.B. Seidler¹; ¹German Aerospace Center (DLR) e.V., Germany
Presenter: Sven Pülm, German Aerospace Center (DLR)
9.1More / Hybrid / Electric Propulsion 1
Chair(s): Fioriti, M.
C 4
05 - Propulsion
05. Sep 22 10:30 11:00 9.1.1 SERIES-HYBRID RETROFIT OF AN XV-15 TILTROTOR AND EMERGENCY PROCEDURE ENERGETIC ANALYSIS
G. Avanzini, University of Salento, Italy; G. Bernardini¹, S. Moretti¹, J. Serafini¹; ¹Roma Tre University, Italy
05. Sep 22 11:00 11:30 9.1.2 DEVELOPMENT OF A CONTROLS APPROACH FOR FUEL CELL-POWERED ALL-ELECTRIC AERO ENGINES BASED ON AN FHA
S. de Graaf¹, S. Kazula¹; ¹DLR e.V., Germany
10.1Aircraft Aerodynamics 1
Chair(s): Mariani, R.
26
03.4 - Applied Aerodynamics
05. Sep 22 10:30 11:00 10.1.1 USING ACTIVE FLOW CONTROL TO IMPROVE THE AERODYNAMIC PERFORMANCE OF THE NEXT GENERATION CIVIL TILT ROTOR AIRCRAFT
J.B. Vos¹, A. Gehri¹, H. Truong², A. Marouf², Y. Hoarau²; ¹CFS Engineering, Switzerland ;²University of Strasbourg, ICUBE Research Institute, France
11.1Design Space Exploration
Chair(s): Pinon Fischer, O., Ireman, T.
27
02 - Systems Engineering and Integration
05. Sep 22 10:30 11:00 11.1.1 A SEMANTIC KNOWLEDGE BASED ENGINEERING FRAMEWORK FOR THE RAPID GENERATION OF NOVEL AIR VEHICLE CONFIGURATIONS
J. Zamboni¹, A. Zamfir¹, E. Moerland¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany
05. Sep 22 11:00 11:30 11.1.2 RULE-BASED VERIFICATION OF A GEOMETRIC DESIGN USING THE CODEX FRAMEWORK
B. Boden¹, Y. Cabac¹, T. Burschyk¹, B. Nagel¹; ¹DLR, Germany
12.1AMAN / DMAN 1
Chair(s): Bauer, T., Mori, R.
24 + 25
09 - Air Transport System Efficiency
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 FOR INTEGRATED ARRIVAL AND DEPARTURE OPERATION OF RUNWAYS
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 QUEUING MODEL
K. Higasa, The University of Tokyo, Japan; E. Itoh, Electronic Navigation Research Institute, Japan
13.1Airworthiness / Certification
Chair(s): Conway, S. R., Krein, A.
35 + 36
10 - Safety and Security
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
B.R. Teixeira¹, L.G.L. de Paula¹, A.C.S. Freitas¹, R.G. Cortes², M.Y.D. Ribeiro², M.M.C. Júnior², E. 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, Q. Ma¹; ¹Beihang University, China
14.1Future Operations
Chair(s): Ying, S.
38
11 - Operations and Sustainment
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 CERTIFICATION
Y.-H. Song¹, X.-L. Zhang¹, Q.-H. Liu, Northwestern Polytechnical University, China; Y.-L. Thang¹; ¹Chinese Flight Test Establishment, China
Reserve Paper 14.1.R A GLOBAL APPROACH TO ASSESSING THE CLIMATE RESILIENCE OF AIRPORTS
M.P.P. Osund-Ireland¹, A.J. Powell¹, C.J. Ireland¹; ¹susteer AB, Sweden

12:00 - 13:00Lunch Break

0.2GL1 “Future Airspace – Meeting Demand Through Integration” Lynne Thompson Hopper, USA
Chair: S. Bagassi ICAS EC member
05. Sep 22 13:00 14:00

1.2Progress toward sustainable aviation (Electrified Propulsion 1) (invited)
Chair(s): Bezos O'Connor, G., Jensen, R.
A1
15 - Guest lectures
05. Sep 22 14:10 14:40 1.2.1 A ROADMAP TOWARDS ENVIRONMENTALLY SUSTAINABLE AVIATION (invited)
B. Loxton, United States
05. Sep 22 14:40 15:10 1.2.2 HYBRID ELECTRIC PROPULSION DEVELOPMENT FOR COMMERCIAL AVIATION
C. Andrews¹, A. Simpson¹; ¹GE, United States
Presenter: Christine Andrews, GE
05. Sep 22 15:10 15:40 1.2.3 TOWARD A COMMUNITY NOISE ASSESSMENT OF SINGLE-AISLE AIRCRAFT WITH HYBRID-ELECTRIC PROPULSION (invited)
M.R. Khorrami, United States
2.2MDAO 2
Chair(s): Rinoie, K.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
05. Sep 22 14:10 14:40 2.2.1 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 4.0 PROJECT
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
3.2UAS 1
Chair(s): Mielosszykk, J.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
05. Sep 22 14:10 14:40 3.2.1 UNMANNED AERIAL VEHICLE – HUMAN PERFORMANCE EVALUTION UNDER CRITICAL OPERATIONAL SCENARIO
E.T. da Silva¹, A.G.P. Sarmento¹, T.R. de Paula¹, A.S. Oliveira¹, J. Possamai¹, H.C. Marques¹, M.M. Cardoso¹, E. Villani¹; ¹Aeronautics 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 COOPERATIVE THREAT ENGAGEMENT WITH HETEROGENEOUS DRONE SWARMS
L. Giacomossi¹, J.A. Ricardo Jr¹, J.F.B. Brancalion, EMBRAER, Brazil; M.R.O.A. Maximo¹, D.A. Santos¹; ¹ITA, Brazil
4.2Hypersonic Aerodynamics
Chair(s): Pezzella, G., Alves, L.
C 1
03.1 - Aerodynamics – CFD Methods and Validation
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 SUPERSONIC/HYPERSONIC CRUISER VEHICLES IN MORE&LESS PROJECT
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 IN HYPERSONIC FLOWS
R.O. Bura, Republic of Indonesia Defense University, Indonesia; F.A. Maulana, Indonesia
5.2GARTEUR 2 (invited)
Chair(s): Blom, A.
C 2
15 - Guest lectures
05. Sep 22 14:10 14:40 5.2.1 THE GROUP OF RESPONSABLES \"FLIGHT MECHANICS, SYSTEMS AND INTEGRATION (GOR FM)\": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES
B. Korn, DLR, Germany; M. Hagström, FOI, Sweden
05. Sep 22 14:40 15:10 5.2.2 THE GROUP OF RESPONSABLES \"ROTORCRAFT (RC-GOR)\": AN OVERVIEW OF ACTIVITIES AND SUCCESS STORIES
A. Visingardi, CIRA, Italy; R. Heger, Airbus Helicopters, Germany; A. Le Pape, ONERA, France; R. Markiewicz, DSTL, United Kingdom; B. Ohlenforst, NLR, Netherlands; K. Pahlke, DLR, Germany; M. White, University of Liverpool, United Kingdom
05. Sep 22 15:10 15:40 5.2.3 AVIATION SECURITY CONCERNS
A. Vozella, Italian Aerospace Research Centre, Italy; P. Bieber, ONERA, France
6.2Experimental Investigations on Vortical Flows
Chair(s): Gibertini, G.
C 3
03.2 - Experimental Aerodynamics
05. Sep 22 14:10 14:40 6.2.1 STRAKE SECTION IMPACT ON HYBRID-DELTA-WING AERODYNAMICS
D. Sedlacek¹, C. Breitamter¹; ¹Technical University of Munich, Germany
05. Sep 22 14:40 15:10 6.2.2 VOLUMETRIC VELOCITY MEASUREMENTS OF A HELICAL VORTEX PAIR
D. Schröder¹, T. Leweke, CNRS, Aix-Marseille Université, Centrale Marseille, France; R. Hörnschemeyer¹, E. Stumpf¹; ¹Institute of Aerospace Systems, RWTH Aachen University, Germany
05. Sep 22 15:10 15:40 6.2.3 NUMERICAL AND EXPERIMENTAL INVESTIGATIONS 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
7.2Composite Damage and Repairs
Chair(s): Kanerva, M., Wright, S.
Bar 5
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
05. Sep 22 14:10 14:40 7.2.1 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.
05. Sep 22 14:40 15:10 7.2.2 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 15:10 15:40 7.2.3 A DAMAGE RECOGNITION METHOD OF COMPOSITE STRUCTURES USING ARTIFICIAL DEFECTIONS
Y. Yang¹, S. Lyu¹; ¹Aircraft Strength Research Institute, China
8.2Aeroelastic Experimental Investigations
Chair(s): Pak, C., Ricci, S.
23
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
05. Sep 22 14:10 14:40 8.2.1 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 14:40 15:10 8.2.2 DESIGN OF AN INNOVATIVE WING TIP FOR AEROELASTIC CONTROL: FROM SCRATCH TO FLIGHT TEST
F. Toffol¹, F. Fonte, Leonardo Helicopters, Italy; S. Ricci¹; ¹Politecnico di Milano, Italy
05. Sep 22 15:10 15:40 8.2.3 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 8.2.R SOME EXPERIMENTAL RESULTS ON DYNAMIC AEROELASTICITY OF PLATES AND SHELLS IN SUBSONIC AND SUPERSONIC FLOW.
J. Lübker, Germany
9.2More / Hybrid / Electric Propulsion 2
Chair(s): Yimer, I.
C 4
05 - Propulsion
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 DEMONSTRATION FLIGHTS OF HYBRID ELECTRIC AIRCRAFT
P. Bohnert, United Kingdom; S.X. Ying, United States; M. Selier, Netherlands
10.2Propulsion Systems
Chair(s): Rogers, M.M., Tai, J.
26
03.4 - Applied Aerodynamics
05. Sep 22 14:10 14:40 10.2.1 TRANSONIC NACELLE DESIGN FOR FUTURE MEDIUM RANGE AERO-ENGINES
B.D.J. Schreiner¹, D.G. MacManus¹, F. Tejero¹, F. Sanchez-Moreno¹, C. Sheaf, Rolls Royce, United Kingdom; ¹Cranfield University, United Kingdom
Presenter: Fernando Tejero, Cranfield University
05. Sep 22 14:40 15:10 10.2.2 STUDY OF EFFECTS ON THE WING\'S AERODYNAMIC CHARACTERISTICS DUE TO DISTRIBUTED PROPULSION OVER WINGSPAN
G.J. Resende¹, V. Malatesta¹, M.C. Savio², B.M. Castro²; ¹ITA - Aeronautics Institute of Technology, Brazil ;²EMBRAER, Brazil
05. Sep 22 15:10 15:40 10.2.3 A NOVEL EMBEDDED INLET BASED ON THE INTEGRATED DESIGN CONCEPT OF FUSELAGE AND INLET
P. Yan, Shenyang Aircraft Design and Research Institute, China; F. Liu, Shenyang Aircraft Design and Research Institute, Chinese Aeronau, China
11.2UAV Navigation 1
Chair(s): Staack, I., Krus, P,
27
06.2 - Flight Dynamics and Control (UAV related)
05. Sep 22 14:10 14:40 11.2.1 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 14:40 15:10 11.2.2 ALTITUDE ESTIMATION BY WIDE-FIELD-INTEGRATION OF OPTIC FLOW
H. Hiraiwa¹, M. Bando¹, S. Hokamoto¹; ¹Kyushu university, Japan
05. Sep 22 15:10 15:40 11.2.3 FIXED-WING UAVS CONTROL WITH MODEL UNCERTAINTIES
M.R. Kartal¹, D. Ignatyev¹, A. Zolotas¹; ¹Cranfield University, United Kingdom
12.2AMAN / DMAN 2
Chair(s): , , Andreeva-Mori, A.
24 + 25
09 - Air Transport System Efficiency
05. Sep 22 14:10 14:40 12.2.1 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 12.2.2 APPLYING MACHINE LEARNING TO TAXI-TIME PREDICTION ATTOKYO INTERNATIONAL AIRPORT
F. Kato¹, E. Itoh¹; ¹The University of Tokyo, Japan
05. Sep 22 15:10 15:40 12.2.3 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, T. Loruenser, AIT Austrian Institute of Technology, Austria; ¹Frequentis AG, Austria
13.2Safety / Security
Chair(s): Weber, G., Toebben, H.
35 + 36
10 - Safety and Security
05. Sep 22 14:10 14:40 13.2.1 LOCALIZATION OF INTERROGATORS WITH A 1030/1090 MHZ SPECTRUM MONITORING SYSTEM
L. Sarperi¹, M. Jäger¹, P. Müller¹, M. Felux¹; ¹ZHAW, Switzerland
Presenter: Michael Jäger, ZHAW School of Engineering
05. Sep 22 14:40 15:10 13.2.2 A FEDERATED LEARNING BASED SECURITY FOR CONTROLLER-PILOT DATA LINK COMMUNICATION
S. Khan¹, G. Singh Gaba¹, A. Gurtov¹; ¹Linköping University, Sweden
Presenter: Suleman Khan, Linköping University
05. Sep 22 15:10 15:40 13.2.3 TECHNICAL CONCEPTS FOR INSPECTING UAVS FOR DAMAGE
J. Eltgen¹, T. Schüppstuhl¹; ¹Hamburg University of Technology, Germany
14.2Sustainment Digitalisation
Chair(s): Gulrez, T., Justin, C.
38
11 - Operations and Sustainment
05. Sep 22 14:10 14:40 14.2.1 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
05. Sep 22 14:40 15:10 14.2.2 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 14.2.3 DIGITAL TWIN CONCEPT FOR AIRCRAFT COMPONENTS
H. Meyer¹, A.-K. Koschlik¹, F. Raddatz¹; ¹German Aerospace Center, Germany
Reserve Paper (interactive) 14.2.R ESTIMATION OF ROTOR IMBALANCE AND MODEL DISCREPANCY USING A BAYESIAN APPROACH
R. Rameshbabu¹, D. Rajaram¹, O.J.P. Fischer¹, D.N. Mavris¹; ¹Georgia Institute of Technology, United States

15:40 - 16:00Break

1.3Future Combat Air Systems – Requirements & Technologies (invited)
Chair(s): Hjelm, J.
A1
15 - Guest lectures
05. Sep 22 16:00 16:30 1.3.1 THE SWEDISH AIR FORCE INTO THE FUTURE – AIMING FOR A HIGHER GROUND AND A SHARPER EDGE (invited)
T. Petersson, Sweden
05. Sep 22 16:30 17:00 1.3.2 FUTURE COMBAT AIRCRAFT SYSTEM THE COMPLEXITY OF THE SKILLS EQUATION (invited)
S. Hopkins, BAE Systems, United Kingdom; I. Noakes, BAe Systems, United Kingdom
05. Sep 22 17:00 17:30 1.3.3 FUTURE COMBAT AIR SYSTEMS: REQUIREMENTS AND TECHNOLOGIES (invited)
G. Girard, France
05. Sep 22 17:30 18:00 1.3.4 POWER/THERMAL 2030 VISION - AIR PLATFORM ELECTRIFICATION (invited)
J.G. Nairus, United States
2.3Technology Assessment
Chair(s): Bagassi, S.
A 2
01.1 - Aircraft Design and Integrated System (Basics and Theory)
05. Sep 22 16:00 16:30 2.3.1 VALIDATION OF SCALED FLIGHT TESTING
P. Schmollgruber¹, C. Toussaint¹, A. Lepage¹, F. Bremmers², H. Jentink², L. Timmermans², N. Genito³, A. Rispoli³, D. Meissner, 5Airbus Operations GmbH, Germany; D. Kierbel, Airbus S.A.S., France; ¹ONERA, France ;²NLR, Netherlands ;³CIRA, Italy
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
C. Jouannet¹, K. Amadori¹, M. Emeneth, PACE America Inc., United States; A. Papageorgiou, Linköpings University, Sweden; ¹Saab Aeronautics, Sweden
3.3UAS 2
Chair(s): Mielosszykk, J.
A 4
01.2 - Aircraft Design and Integrated System (Applications)
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
4.3Assessment of Unconventional Aircraft Configurations Through MDO (invited)
Chair(s): Rinoie, K., Zingg, D.
C 1
15 - Guest lectures
05. Sep 22 16:00 16:30 4.3.1 A MULTIFIDELITY MULTIDISCIPLINARY APPROACH TO UNCONVENTIONAL AIRCRAFT DEVELOPMENT AND ASSESSMENT WITH APPLICATION TO THE STRUT-BRACED-WING AND HYBRID-WING-BODY CONFIGURATIONS
D.W. Zingg¹, T. Chau¹, A.L. Gray¹, T.A. Reist¹; ¹University of Toronto Institute for Aerospace Studies, Canada
05. Sep 22 16:30 17:00 4.3.2 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 4.3.3 MDAO OF A TRANSONIC TRUSS-BRACED WING VISION VEHICLE
D.S. Lazzara¹, N.A. Harrison¹; ¹Boeing, United States
05. Sep 22 17:30 18:00 4.3.4 APPLICATION OF AERODYNAMIC AND AERO-STRUCTURAL OPTIMIZATION FOR ENERGY EFFICIENT AIRCRAFT (invited)
O. Brodersen, Germany; T. Wunderlich, Germany; M. Abu-Zurayk, Germany; S. Görtz, Germany; C. Ilic, Germany; L. Reimer, Germany
5.3Actuation Systems
Chair(s): Stumpf, E., Krus, P.
C 2
07 - Systems, Subsystems and Equipment
05. Sep 22 16:00 16:30 5.3.1 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 5.3.2 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 5.3.3 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 5.3.4 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
6.3Aeroacustic Measurements
Chair(s): Aschwanden, P.
C 3
03.2 - Experimental Aerodynamics
05. Sep 22 16:00 16:30 6.3.1 AERODYNAMIC AND AEROACOUSTIC CHARACTERISTICS OF THE NACA 0008 AIRFOIL
F.L. dos Santos¹, L. Botero-Bolivar¹, C.H. Venner¹, L.D. de Santana¹; ¹University of Twente, Netherlands
05. Sep 22 16:30 17:00 6.3.2 EXPERIMENTAL STUDIES ON THE INTERACTION BETWEEN PROPELLERS AND WING
G.P.G. Silva¹, M.V.R.J. Silva¹, J.P. Eguea¹, F.M. Catalano¹; ¹Department of Aeronautical Engineering, University of Sao Paulo, Brazil
05. Sep 22 17:00 17:30 6.3.3 IDENTIFICATION OF CRITICAL ACOUSTIC MODES FOR AN OPEN BOX CAVITY WITH ADJUSTABLE DEPTH
S. Hammer¹, J. Fridh¹, M. Billson, GKN Aerospace Sweden, Sweden; ¹KTH Royal Institute of Technology, Sweden
Presenter: Jens Fridh, KTH Royal Institute of Technology
05. Sep 22 17:30 18:00 6.3.4 AN OVERVIEW OF AERO-ACOUSTIC EXPERIMENTAL TECHNOLOGY IN AVIC FL-10 WIND TUNNEL
Z. Guocheng¹, B. Anyu ¹, C. Bao¹, L. Xiangnan¹; ¹AVIC ARI, China
Presenter: BAO Anyu, AVIC ARI
7.3Advances in Aerostructures
Chair(s): Bayandor, J.
Bar 5
04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
05. Sep 22 16:00 16:30 7.3.1 TOWARDS VIRTUAL FATIGUE TESTING: DEVELOPMENTS AND CHALLENGES FOR METALLIC AND COMPOSITES AEROSTRUCTURES
I. Rivero¹, A. Palomar¹, N. Martin¹, M. Lozano¹, J. Romero¹, B. De Nicolas¹, M. Rebollo¹, J. Gomez-Escalonilla¹; ¹Airbus, Spain
Presenter: Zuriñe Mujika
05. Sep 22 16:30 17:00 7.3.2 VARIATIONS IN STRUCTURAL PROPERTIES OF LATTICE STRUCTURES DEPENDING ON UNIT CELL SHAPE FOR MORPHING WINGS
Y. Nishijima¹, H. Tanaka¹, A. Biron, Special Military School of Saint-Cyr, France; T. Miura¹; ¹National Defense Academy, Japan
05. Sep 22 17:00 17:30 7.3.3 PROPOSITION OF A NEW QUALIFICATION IMPACT TEST FOR AEROSPACE SMART STRUCTURES
G. Gastaldo, France; Y. Rafik, France; M. Budinger, France; V. Pommier-Budinger, France; P. Olivier, France; P. Navarro, France
05. Sep 22 17:30 18:00 7.3.4 PERIDYNAMIC SIMULATION PLATTFORM TO DETERMINE VIRTUAL ALLOWABLES OF MANUFACTURING DEVIATIONS
C. Willberg¹, J.-T. Hesse¹, D. Krause¹; ¹German Aerospace Center, Germany
8.3Computational Aeroelasticity
Chair(s): Ricci, S., Nitzsche, F.
23
04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
05. Sep 22 16:00 16:30 8.3.1 AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO AND STRUT-BRACED WINGS
Y. Le Lamer¹, J. Morlier, ICA, Université de Toulouse, ISAE-SUPAERO, MINES ALBI, UPS, INSA, France; E. Benard¹, P. He, Iowa State University, United States; ¹ISAE-SUPAERO, Université de Toulouse, France
05. Sep 22 16:30 17:00 8.3.2 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 17:00 17:30 8.3.3 NUMERICAL INVESTIGATION ON THE DOUBLE TRANSONIC DIP OF SUPERCRITICAL AIRFOIL FLUTTER
T. Miyake¹, H. Terashima¹; ¹Hokkaido University, Japan
05. Sep 22 17:30 18:00 8.3.4 ANALYSIS OF THE HAMMERHEAD LAUNCH VEHICLE USING CFD-CAE COUPLED METHOD IN THE TRANSONIC REGION
H.-G. Rho, Korea Aerospace Univeristy, South Korea; P.A. Nguyen¹, J.-S. Bae¹, S.-H. Park, Konkuk University, South Korea; K.-H. Byun, Korea Agency for Defense Development, South Korea; ¹Korea Aerospace University, Vietnam
Reserve Paper (interactive) 8.3.R A NUMERICAL METHOD FOR STUDY ON THE AERO-ELASTICITY OF AIR-TO-AIR MISSILES 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
9.3MDO for Collaborative Propulsion Design
Chair(s): Thomas, R.
C 4
05 - Propulsion
05. Sep 22 16:00 16:30 9.3.1 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
05. Sep 22 16:30 17:00 9.3.2 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 17:00 17:30 9.3.3 KNOWLEDGE-BASED CONCEPTUAL DESIGN METHODS FOR GEOMETRY AND MASS ESTIMATION OF RUBBER AERO ENGINES
J. Häßy¹, J. Schmeink¹; ¹DLR, Germany
05. Sep 22 17:30 18:00 9.3.4 MULTIDISCIPLINARY OPTIMIZATION OF COMBUSTION CHAMBER FOR SMALL GAS TURBINE ENGINES
C.-A. Pham¹, Q.-H. Nguyen¹, T.-A. Vu¹, N.-V. Nguyen¹; ¹Viettel Aerospace Institute, Viettel Group, Vietnam
Presenter: Nhu-Van Nguyen, Viettel Aerospace Institute, Viettel Group
10.3Flight Modelling and Simulation 1
Chair(s): Kim, S.
26
06.1 - Flight Dynamics and Control (Control & Modelling)
05. Sep 22 16:00 16:30 10.3.1 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 10.3.2 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 10.3.3 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 10.3.4 DEEP REINFORCEMENT LEARNING FOR EVTOL HOVERING CONTROL
D.S. Alarcon¹, J.H. Bidinotto¹; ¹University of São Paulo, Brazil
11.3UAV Control and AI
Chair(s): Rogalski, T., Bil, C.
27
06.2 - Flight Dynamics and Control (UAV related)
05. Sep 22 16:00 16:30 11.3.1 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 16:30 17:00 11.3.2 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 17:00 17:30 11.3.3 USING DEEP REINFORCEMENT LEARNING TO IMPROVE THE ROBUSTNESS OF UAV LATERAL-DIRECTIONAL CONTROL
R. Wang¹, Z. Zhou¹, X. Zhu¹, L. Zheng, Delft University of Technology, Netherlands; ¹Northwestern Polytechnical University, China
12.3Climate / Environment Impacts
Chair(s): Matayoshi, N., Eek, M.
24 + 25
09 - Air Transport System Efficiency
05. Sep 22 16:00 16:30 12.3.1 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 12.3.2 A COMPARISON OF CLIMATE-OPTIMISED AND FUEL-OPTIMISED INTERMEDIATE STOP OPERATIONS FOR SELECTED CASE STUDIES
Z. Zengerling¹, F. Linke¹, C. Weder¹, K. Dahlmann¹; ¹Deutsches Zentrum für Luft- und Raumfahrt, Germany
05. Sep 22 17:00 17:30 12.3.3 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 12.3.4 AN ENGINELESS TAXI OPERATIONS SYSTEM USING BATTERY-OPERATED AUTONOMOUS TOW TRUCKS
S. Zaninotto¹, J. Gauci¹, B. Zammit¹; ¹University of Malta, Malta
13.3UAV/UAM
Chair(s): Boucher, A., Consiglio, M.C.
35 + 36
10 - Safety and Security
05. Sep 22 16:00 16:30 13.3.1 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 13.3.2 URBAN AIR TRAFFIC MANAGEMENT FOR COLLISION AVOIDANCE WITH NON-COOPERATIVE 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 13.3.3 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 13.3.4 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 13.3.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
Presenter: Aditya Devta, Technical University of Munich
14.3Operations Optimisation
Chair(s): Kelly, M., Olsson, E.
38
11 - Operations and Sustainment
05. Sep 22 16:00 16:30 14.3.1 THE ALBATROSS PROJECT – A EUROPEAN INITIATIVE TO REDUCE AVIATION’S CARBON DIOXIDE EMISSIONS IN LARGE SCALE
F. Sachs¹, F. Abdelmoula¹, D. Vechtel¹; ¹DLR, Germany
Presenter: Dennis Vechtel, DLR
05. Sep 22 16:30 17:00 14.3.2 ZERO-EMISSION REGIONAL AVIATION IN SWEDEN
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 14.3.3 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 14.3.4 AERODYNAMIC INVESTIGATION OF VERY CLOSELY FLYING FIGHTERS TO DEVELOP NEW FORMATION TYPES
S.M. Aydin¹, A.G. Yavuz, Turkish Aerospace Industries, Turkey; M. Kaya¹; ¹Yildirim Beyazit University, Turkey