30th Congress of the International Council of the Aeronautical Sciences

Preliminary Programme - Interactive Presentations

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ACCEPTED PAPERS - CATEGORY C - INTERACTIVE PRESENTATIONS

These papers will be presented in the Interactive Presentations area
Most papers will also appear in the Congress CD Proceedings



1 - Aircraft Design and Integrated Systems

ICAS2018-P1.1: MARCO GEHLEN╣, PAULO TADEU DE MELLO LOURENCAO╣, LU═S GONZAGA TRABASSO, ITA, Brazil; ╣EMBRAER S.A., Brazil
EDUCATING ENGINEERS FOR THE DEVELOPMENT OF PRODUCT SERVICE SYSTEMS (PSS)
ICAS2018-P1.2: R.C. Munjulury, Link÷ping University, Sweden
KNOWLEDGE-BASED AUTOMATIC ROUTING FOR AIRCRAFT SYSTEMS
ICAS2018-P1.3: S.-M. Hong╣, M.-J. Tahk╣; ╣KAIST, South Korea
MULTISTAGE MISSILE TRAJECTORY AND STAGE OPTIMIZATION VIA DELTA-V APPROACH
ICAS2018-P1.4: H Zhang╣, B.F Song╣, H Ma╣, W Fang╣; ╣ School of Aeronautics, Northwestern Polytechnical University, China
ANALYSIS AND OPTIMIZATION OF ANTI-WIND CAPABILITY OF AN ELECTRIC HYBRID AERIAL VEHICLE
ICAS2018-P1.5: H. L. H. D. Lemos, Universidade Federal de Minas Gerais, Brazil
ENDURANCE OPTIMIZATION OF AN ELETRIC UNMMANED AERIAL VEHICLE
ICAS2018-P1.6: J.M. Souza╣, F.M. Catalano╣; ╣University of SŃo Paulo, Brazil
MULTI-DISCIPLINARY DESIGN OPTIMIZATION OF A BLENDED WINGLET
ICAS2018-P1.7: Yoonpyo Hong╣, Dongyeon Han╣, Kwanjung Yee╣; ╣Seoul National University, South Korea
DESIGN PARAMETER STUDY OF DRONE BLADE CONSIDERING AEROACOUSTICS
ICAS2018-P1.8: Xiaoxiao He, Aviation Industry Development Research Center of China, China
STUDY ON RADRA CROSS SECTION FOR FLYING-WING UUMANNED AERIAL VEHICLE WITH CLOSE FORMATION FLIGHT
ICAS2018-P1.9: A Abdalla╣, H D Cerˇn-Mu˝oz╣, F Catalano ╣; ╣EESC-USP, Brazil
DESIGN AND PERFORMANCE ASSESSMENT OF AN INVERTED RECTANGULAR DORSAL INTAKE FOR MILITARY AVIATION
ICAS2018-P1.10: L.-J. PAN, Shanghai Aircraft Design and Research Institute, China
PRELIMINARY DESIGN FOR A LOW REYNOLDS NUMBER BWB UAV DEMONSTRATOR
ICAS2018-P1.11: N. Vidanovic, University of Belgrade, Faculty of Transport and Traffic Enginee, Serbia; Bosko Rasuo, University of Belgrade, Faculty of Mechanical Engineering, Serbia; G. Kastratovic, University of Belgrade, elgrade, Faculty of Transport and Traffi, Serbia
MULTI-DISCIPLINARY MISSILE FIN OPTIMIZATION
ICAS2018-P1.12: Liu Jianyan, AVIC the First Aircraft Institute, China
RESEARCH ON SHAPE STEALTH OF THE MILITARY AIRCRAFT

2 - Systems Engineering and Integration

ICAS2018-P2.1: JCM Marques, EMBRAER, Brazil
USING SOFTWARE SAFETY STANDARDS FOR MEDICAL DEVICE IN AVIATION EMBEDDED SOFTWARE DEVELOPMENT
ICAS2018-P2.2: M Ribeiro, ITA, Brazil
SOLAR POWERED UAV: TERRAIN FOLLOW AIRCRAFT ATTITUDE IMPACTS ON CONCEPTUAL DESIGN
ICAS2018-P2.3: L. Ribeiro, Brazil
STAMP METHOD APPLICATION ON INDUSTRIAL MANAGEMENT
ICAS2018-P2.4: Bin Wu╣, Xudong Qiu╣, Feng Fang╣, Zhichao Yao╣; ╣COMAC Shanghai Aircraft Design and Research Institute, China
CIVIL AIRCRAFT DEVELOPMENT PROJECT IPT TEAM OBS DEVELOPMENT RESEARCH

3.1 - Aerodynamics - CFD Methods and Validation

ICAS2018-P3.1.1: M.M. Hoffmann, Argentinian Air Force, Argentina
AERODYNAMICS, FLIGHT PERFORMANCE AND DYNAMICS OF AN UNMANNED AERIAL VEHICLE
ICAS2018-P3.1.2: Guangping Qian╣, Dawei Wu╣, Chao Ma╣; ╣COMAC, China
NUMERICAL STUDY OF VARIABLE CAMBER WING EFFECT ON AERODYNAMIC PERFORMANCE FOR LONG RANGE CIVIL AIRCRAFT
ICAS2018-P3.1.3: W.K. Amaral Silva, Instituto Tecnolˇgico de Aeronßutica, Brazil
CALCULATION OF THE EFFICIENCY OF A RADIAL TURBINE CONSIDERING THE HEAT LOSS FROM ITS VOLUTE
ICAS2018-P3.1.4: Guangping Qian╣, Jiangtao Si╣, Kaili Liu╣; ╣COMAC, China
NUMERICAL STUDY OF REYNOLDS NUMBER EFFECT ON AERODYNAMIC LOAD OF CIVIL AIRCRAFT
ICAS2018-P3.1.5: N Gautier╣, N Manzanares-Filho╣, E-R Da Silva╣; ╣UNIFEI, Brazil
COMPARISON AND APPLICATION OF DIFFERENT TECHNIQUES OF MULTI-OBJECTIVE OPTIMIZATION FOR AERODYNAMICS WINGS DESIGN
ICAS2018-P3.1.6: J.A.S. Oliveira de Souza Oliveira, UFMG, Brazil
COMPARISON AND VALIDATION OF TURBULENCE MODELS FOR VORTEX GENERATORS AERODYNAMIC AND HEAT TRANSFER PREDICTION
ICAS2018-P3.1.7: D. HAN╣, J.Y. Huh╣, K.H. Kim╣; ╣Seoul National University, South Korea
ANALYSIS OF HYPERSONIC FLOW AND STRUCTURAL THERMAL RESPONSE USING A MESHLESS METHOD

3.2 - Experimental Aerodynamics

ICAS2018-P3.2.1: Dj. Vukovic╣, V. Lapcevic╣, D. Marinkovski╣, M. Samardzic╣, L. Petrovic╣; ╣Military technical institute (VTI), Serbia
DIGITALIZATION OF INTERNAL WIND TUNNEL BALANCES
ICAS2018-P3.2.2: LO Ferreira, Airship do Brasil, Brazil
A SIMILITUDE METHOD FOR AIRSHIP WIND TUNNEL SCALE TESTING
ICAS2018-P3.2.3: D. Damljanovic╣, Dj Vukovic╣, G. Ocokoljic╣, J. Isakovic, College of Applied Engineering Studies , Serbia; B. Rasuo, Faculty of mechanical Engineering, Serbia; ╣Military technical institute (VTI), Serbia
CONVERGENCE OF TRANSONIC WIND TUNNEL TEST RESULTS OF THE AGARD-B STANDARD MODEL
ICAS2018-P3.2.4: G. Ocokoljic, Military Technical Institute, Belgrade, Serbia
EXPERIMENTAL RESEARCH AND NUMERICAL ANALYSIS OF COLD AND HOT-JET SIMULATION OF TRUST VECTOR CONTROL BY JET TABS
ICAS2018-P3.2.5: E.E.Son Son, Joint Institute for High Temperature RAS, Russia
HIGH-PRESSURE IGNITION PLASMA TORCH FOR HYPERSONIC TESTING

3.3 - Basic Fluid Dynamics and Flow Control

ICAS2018-P3.3.1: Li Li, Beijing Aeronautical Science & Technology Research Institute, China
INVESTIGATION ON THE EFFECTS OF PLASMA FLOW CONTROL ON AIRFOILS

3.4 - Applied Aerodynamics

ICAS2018-P3.4.1: R. R. P. P. Pereira, IAE, Brazil
STATISTICAL ANALYSIS OF OPENING FORCES IN PARACHUTES
ICAS2018-P3.4.2: Taekeun Yoon, South Korea; Kwanjung Yee, South Korea
DESIGN OPTIMIZATION OF AIRFOIL CONSIDERING ICE ACCRETION AND WIND TURBINE NOISE
ICAS2018-P3.4.3: J Cecrdle╣, Z Pßtek╣, R Kulhßnek╣, P Vrchota╣, N Äi×kovskř╣; ╣VZL┌, a.s., Czech Republic
EXPERIMENTAL AND CFD STUDY OF KRUEGER FLAPS
ICAS2018-P3.4.4: V. Vid╣, A. Zamyatin╣, V. Rogozin╣, M. Grigorev╣, S. Zuev╣, A. Zhelannikov▓, O. Tkachenko▓, V. Dorin, SC "Kamov", Russia; ╣Gromov FRI, Russia; ▓TsAGI, Russia
AERODYNAMIC COMPATIBILITY OF FLYING VEHICLES DURING TAKE-OFF AND LANDING OPERATIONS AT DIFFERENT AIRFIELDS (OBJECTS)
ICAS2018-P3.4.5: L. Barbosa, Condax Tecnologia, Brazil
A SOARING AIRCRAFT CONCEPTUAL DESIGN, STARTING FROM HISTORICAL PERSPECTIVE AND ANALYSIS.
ICAS2018-P3.4.6: M.-K. Kowalski, Air Force Institute of Technology, Poland
AERODYNAMIC COEFFICIENT PREDICTION OF MICRO AERIAL VEHICLE USING NEURAL NETWORK
ICAS2018-P3.4.7: T. Melin, Svenska Flygtekniska Institutet, Sweden; A.A. Gastaldi╣, M. Zhang╣; ╣Airinnova, Sweden
IMPLEMENTATION OF A VORTEX LATTICE METHOD IN A HETEROGENEOUS PROGRAMMING LANGUAGE ENVIRONMENT
ICAS2018-P3.4.8: Guilherme Souza Papini, UFMG, Brazil; Sergio Esteban Roncero, University of Seville, Spain
AERODYNAMICS ANALYSIS OF A UAV TILT ROTOR IN WIND TUNNEL AND CFD
ICAS2018-P3.4.9: O. J. Kwon, KAIST, South Korea
NUMERICAL INVESTIGATION OF BUFFET CHARACTERISTICS OF A DELTA WING CONFIGURATION AT HIGH ANGLES OF ATTACK
ICAS2018-P3.4.10: G. B. Campos╣, J. T. Tomita╣, F. P. Costa╣, C. Bringhenti╣, O. Petit▓, T. Gronstedt▓, A. C. Patrao▓, G. Trapp│, C. R. I. Silva│, A. Lundbladh, GKN, Sweden; ╣Instituto Tecnolˇgico de Aeronßutica, Brazil; ▓Chalmers, Sweden; │Embraer, Brazil
PROPULSIVE EFFICIENCY OF BOUNDARY LAYER INGESTION PROPELLERS
ICAS2018-P3.4.11: A. A. F. Barbosa╣, F. M. Catalano╣; ╣University of Sao Paulo (EESC-USP), Brazil
INFLUENCE OF GULL WING ON LONGITUDINAL AND LATERAL-DIRECTIONAL COEFFICIENTES OF AN AIRPLANE
ICAS2018-P3.4.12: Y.L. Zheng╣, Q.L. Qu╣, P.Q. Liu╣; ╣Beihang University, China
HIGH LIFT MECHANISM OF A 2D FLAPPING WING IN HOVERING FLIGHT
ICAS2018-P3.4.13: J.A.S. Oliveira de Souza Oliveira, UFMG, Brazil
ON THE EFFECTS OF GEOMETRY AND FLOW CONDITIONS ON THE EFFICIENCY OF PERIODIC RIB VORTEX GENERATORS AS HEAT EXCHANGERS

4.1 - Material Issues, Fatigue and Damage Tolerance

ICAS2018-P4.1.1: qian wang, The Research Institute for Special Structures of Aeronautical Co, China; junxia tian, he Research Institute for Special Structures of Aeronautical Com, China
EFFECT OF DIELECTRIC PROPERTIES DUE TO THE CHANGE OF DIELECTRIC AS A RESULT OF ELEVATORY TEMPERATURE
ICAS2018-P4.1.2: B. L. Nolli╣, A. T. A. Melo╣, C. A. Cimini Junior╣; ╣UFMG, Brazil
CRACK PROPAGATION STARTING AT HOLEĺS EDGE GROWING TO PLATEĺS MAJOR DIMENSION USING FEM
ICAS2018-P4.1.3: I. Skhabovskyi, Federal University of Uberlandia, Brazil
IOSIPESCU SHEAR TESTING OF FIBER-METAL LAMINATE PANELS REINFORCED WITH METAL PINS DEPOSITED BY CMT WELDING
ICAS2018-P4.1.4: R.M.V. Campos, Universidade Catˇlica de Minas Gerais, Brazil; A.C.F. Santos╣, T.V.D.C. Avelar╣, B.M.A. Ferreira╣, L.F.T. Rocha╣, P.H.S. Maia╣, S.F.M.A. Barbosa╣, S.O. Figueiredo╣, T.A.A. Khoury╣, V.L.D. Mendonša╣, E.C. Lemos╣; ╣Universidade Catˇlica de Minas Gerais, Brazil
COMPARATIVE STUDY AND VALIDATION OF MATERIAL WITH BETTER PERFORMANCE IN TERMS OF THERMAL ABSORPTION INSIDE AN AIRCRAFT
ICAS2018-P4.1.5: A. T. A. MELO╣, B. L. NOLLI╣, C. A. CIMINI JR╣; ╣Universidade Federal de Minas Gerais, Brazil
FINITE ELEMENT MODEL DEVELOPMENT FOR SIMULTANEOUS CRACK PROPAGATION IN TWO COOPERATIVE LUGS

4.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity

ICAS2018-P4.2.1: L.A. Magerramova╣, M.E. Volkov╣, A.I. Afonin╣, M.S. Svinareva╣, D.V. Kalinin╣; ╣CIAM, Russia
THE USE OF LIGHTWEIGHT LATTICE STRUCTURES FOR FAN BLADES OF GAS TURBINE ENGINES
ICAS2018-P4.2.2: V.-A.-S.M. Paiva╣, P.-R-G. Kurka╣, J.-H. Izuka, UNICAMP - FCA, Brazil; ╣UNICAMP - FEM, Brazil
KINEMATICS AND DYNAMICS OF A TENSEGRITY STRUCTURE IN EXPANSION
ICAS2018-P4.2.3: F. Goncalves Garcia, Embraer, Brazil
PRELIMINARY CONSIDERATIONS ABOUT THE INFLUENCE OF THE MACHINING RADIUS ON BUCKLING OF INTEGRALLY STIFFENED PANELS
ICAS2018-P4.2.4: G. S. R Rodrigues, PUC-Rio, Brazil
STRUCTURAL INTEGRITY ANALYSIS DUE TO IMPACT BETWEEN TWO SOLID BODIES
ICAS2018-P4.2.5: L. Barbosa, Condax Tecnologia, Brazil
COMPROMISE BETWEEN AERODYNAMIC, STABILITY, STRUCTURE STANDPOINTS IN A HIGH-ASPECT RATIO AIRCRAFT DESIGN
ICAS2018-P4.2.6: D Andrade╣, W Corbelli╣, R Martins╣, R Queiroz╣; ╣Universidade Federal de Minas Gerais, Brazil
STRUCTURAL DESIGN OF AN UAV FUSELAGE USING TOPOLOGY OPTIMIZATION METHODS
ICAS2018-P4.2.7: R. S. Martins╣, M. T. Santos, Embraer, Brazil; E. S. Palma╣; ╣UFMG, Brazil
FASTENING ANALYSIS USING BOTH HIGH AND LOW FIDELITY FINITE ELEMENT MODELS
ICAS2018-P4.2.8: L.M.B.C. Campos, Instituto Superior Tecnico, Portugal
ON THE NON-LINEAR COUPLING OF BENDING AND IN-PLANE STRESSES IN AN ELASTIC PLATE
ICAS2018-P4.2.9: J.R. Banerjee, City, University of London, United Kingdom
THE EFFECTS OF FUSELAGE MASS AND INERTIA ON THE FLUTTER CHARACTRISTICS OF TRANSPORT AIRCRAFT
ICAS2018-P4.2.10: M. HL Mou, Tianjin Key Laboratory of Civil Aircraft Airworthiness and Maint, China
RESEARCH ON CRASHWORTHINESS OF TYPICAL CIVIL AIRCRAFT SUB-CARGO FUSELAGE SECTION
ICAS2018-P4.2.11: F. A. Fenelon╣, G. F. S. Neves╣, R. S. Martins╣; ╣Universidade Federal de Minas Gerais, Brazil
STRUCTURAL OPTIMIZATION AND PROPOSITION OF PRE-SIZING PARAMETERS FOR UAVS WING SPARS
ICAS2018-P4.2.12: M. Wojtas╣, ? Czajkowski╣, T. Szczepanik╣; ╣Institute of Aviation, Poland
NEW TECHNOLOGY OF LAYERED STRUCTURES IMPLEMENTED IN SELECTED GYROPLANE COMPONENTS
ICAS2018-P4.2.13: YKJ KAIJUN, The First Aircraft Institute of the Aviation Industry Corporatio, China
THE ANALYSIS AND RESEARCH OF AIRCRAFT NOSE LANDING GEAR BAY DAMAGE
ICAS2018-P4.2.14: SH.-X. Jia, Northwestern Polytechnical University, China
FLEXIBLE ROTOR OPTIMIZATION DESIGN WITH CONSIDERING THE UNCERTAINTY OF RESIDUAL UNBALANCED MASS
ICAS2018-P4.2.15: S. Tashi, Aerospace Eng Dept, Sharif Uni of Tech, Iran
GA OPTIMIZATION OF SCARF JOINT FOR A REPAIR WITH DIFFERENT STACKING SEQUENCE TO STRUCTURE CONSIDERING NONLINEAR ADHESIVE
ICAS2018-P4.2.16: A. Mazidi, Iran
FLUTTER OF A 3DOF AIRFOIL CARRYING, ELASTICALLY, AN UNBALANCE ENGINE

5 - Propulsion

ICAS2018-P5.1: Jie-fei Sui, COMAC, China
THRUST REVERSER INADVERTENT DEPLOYMENT IMPACT STUDY ON AIRPLANE CONTROLLABILITY
ICAS2018-P5.2: O.E. Egorov, CIAM, Russia
DEVELOPMENT OF THE TECHNICAL CONCEPT OF THE REVERSING/VECTORING DEVICE FOR HIGH BYPASS RATIO ENGINES
ICAS2018-P5.3: F.D. Golberg╣, O.S. Gurevich╣, A.A. Petukhov╣; ╣CIAM, Russia
IDENTIFICATION METHOD OF THE SIMULATION MODEL ôVIRTUAL ENGINEö BUILT INTO THE DIGITAL ENGINE CONTROL SYSTEM
ICAS2018-P5.4: L.E. van den Ende╣, Q. Li╣, F. Avallone╣, D. Casalino╣, G. Eitelberg╣, L.L.M. Veldhuis╣; ╣Delft University of Technology, Netherlands
SWIRL RECOVERY DESIGN FOR INSTALLED PROPELLER PROPULSION SYSTEMS
ICAS2018-P5.5: X.D. Yang, China; Z.B. Liu, China; S.L. Zhang, China; C. Song, China
AERODYNAMIC DESIGN OF KEY COMPONENTS OF THE LARGE-DISCHARGE AXIAL FAN AT HIGH ALTITUDE
ICAS2018-P5.6: Xinying Liu╣, Leonardo Manfriani╣, Flavio Ferrari╣; ╣Zurich University for Applied Science, Switzerland
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF COOLING CONCEPT FOR AN ELECTRIC PROPULSION SYSTEM FOR AEROBATIC AIRCRAFT
ICAS2018-P5.7: D. V. Kalinin╣, L.A. Magerramova╣; ╣CIAM, Russia
DYNAMIC MODEL FOR PLANETARY GEAR SETS OF GEARED TURBOFAN JET ENGINES
ICAS2018-P5.8: A. Gulienko╣, O. Gurevich╣, M. Gordin╣; ╣CIAM, Russia
CHARACTERISTICS OF SYSTEMS WITH ELECTRICALLY DRIVEN UNITS - EXPERIMENTAL STUDIES IN A GAS TURBINE ENGINE DEMONSTRATOR
ICAS2018-P5.9: V. Talyzin, TsAGI, Russia
INVESTIGATION OF THE EXTERNAL DRAG OF THE NON-AXISYMMETRIC AFTERBODIES
ICAS2018-P5.10: V.Yu. Aleksandrov╣, M.V. Ananyan, MIPT, Russia; K.Yu. Arefyev╣, O.D. Dikova▓, A.N. Prokhorov╣, K.V. Fedotova▓, L.S. Yanovskiy╣; ╣CIAM, Russia; ▓BMSTU, Russia
INVESTIGATION OF THE PROCESS SUBLIMATION FOR SOLID HYDROCARBONICS IN PERMANENT SECTION CHANNELS

6.1 - Flight Dynamics and Control (Control & Modelling)

ICAS2018-P6.1.1: K. H. Kienitz, ITA, Brazil; P. A. V. Torres, Embraer, Brazil
ANALYSIS OF ROBUST STABILITY AND ROBUST PERFORMANCE OF MIMO FLIGHT CONTROL LAW USING STRUTURED SINGULAR VALUE
ICAS2018-P6.1.2: T Silva, Embraer, Brazil
TIRE-GROUND INTERACTION FORCES AND MOMENTS FOR VMCG DYNAMIC MODELLING
ICAS2018-P6.1.3: Natan Viana╣, Karl Heinz Kienitz╣; ╣ITA, Brazil
ON RELAXED ROLL CONTROL SCHEMES FOR LAUNCHING VEHICLES
ICAS2018-P6.1.4: T. Rogalski╣, A. Tomczyk╣; ╣Rzeszˇw University of Technology, Poland
APPLICATION OF THE DISTURBANCE VALUE MEASURED DURING THE REAL FLIGHT TO THE FLIGHT CONTROL SYSTEM SYNTHESIS

6.2 - Flight Dynamics and Control (UAV related)

ICAS2018-P6.2.1: M.E. El-Salamony, Moscow Institute of Physics and Technology, Russia
ON DISTURBED MOTION NATURAL FREQUENCIES VALIDATION OF SMALL UAVS
ICAS2018-P6.2.2: J. Theron╣, L. Dala, Northumbria University Newcastle, United Kingdom; D. N. Wilke╣, P. Barrier, UAS consultant, South Africa; ╣University of Pretoria, South Africa
PRACTICAL IMPLEMENTATION OF A TRAJECTORY PLANNING ALGORITHM FOR AN AUTONOMOUS UAV
ICAS2018-P6.2.3: J.-W. Lee╣, Anh Tuan Nguyen, Le Quy Don Technical University , Vietnam; J.-H. Han╣; ╣KAIST, South Korea
LONGITUDINAL FLIGHT CONTROL OF BIOINSPIRED FLAPPING-WING MICRO AIR VEHICLE WITH EXTENDED UNSTEADY VORTEX-LATTICE METHOD.
ICAS2018-P6.2.4: F.M.M Machini Malachias Marques, Universidade Federal de UberlÔndia, Brazil
DEVELOPMENT OF A DIGITAL SIGNAL PROCESSING WORKBENCH AND HARDWARE INTEGRATION FOR A ROTARY-WING UNMANNED AIRCRAFT

7 - Systems, Subsystems and Equipment

ICAS2018-P7.1: D. H. Arjoni╣, E. Villani╣, M. RodrÝguez╣, A. M. Matheus╣, A. Almeida╣, G. Rocha╣, L. G. Trabasso╣, D. Hidalgo, UPB, Colombia; ╣ITA, Brazil
WORKLOAD MEASUREMENT AND INFLUENCE ON PILOT PERFORMANCE IN THE SIVOR FLIGHT SIMULATOR ENVIRONMENT
ICAS2018-P7.2: A Sanches, Aeronautics Institute of Technology , Brazil
DESIGNING A VISION-BASED SYSTEM TO MEASURE IN-FLIGHT WING DEFORMATION
ICAS2018-P7.3: A. G. Gardi, RMIT University, Australia
A NOVEL MULTI-SENSOR SYSTEM FOR EARLY-DETECTION OF PLANT PESTS AND DISEASES FROM UNMANNED AIRCRAFT
ICAS2018-P7.4: J. Schminder╣, R. Hńllqvist▓, M. Eek▓, R. Gňrdhagen╣; ╣Link÷ping University, Sweden; ▓Saab Aeronautics, Sweden
PILOT PERFORMANCE AND HEAT STRESS ASSESSMENT SUPPORT USING A COCKPIT THERMOREGULATORY SIMULATION MODEL
ICAS2018-P7.5: F. Lucchi╣, S. Bagassi╣, F. De Crescenzio╣; ╣University of Bologna, Italy
DESIGN FOR COMFORT: AIRCRAFT INTERIORS DESIGN ASSESSMENT THROUGH A HUMAN CENTERED RESPONSE MODEL APPROACH
ICAS2018-P7.6: J.P. Kang╣, G.J. Shim╣, K.J. Yee╣; ╣Seoul national university, South Korea
COST-EFFECTIVE TRACKING, TELEMETRY AND COMMAND SYSTEM DEVELOPMENT FOR HIGH-ALTITUDE SCIENTIFIC BALLOON.

8 - Manufacturing and Supply Chain Management

ICAS2018-P8.1: Ping Xu╣, Xiangming Wang╣, Shiquan Bi╣, Hao Cui╣; ╣Shenyang Aircraft Design and Resesarch Institute, China
APPLICATION RESEARCH OF LARGE COMPLICATED FRAME BEAM INTEGRAL COMPONENT BASED ON ELECTRON BEAM ADDITIVE MANUFACTURING

9 - Air Transport System Efficiency

ICAS2018-P9.1: SÚrgio MourŃo╣, Kerley Oliveira╣; ╣University Center UNA, Brazil
THE PRIVATE MANAGEMENT OF BRAZILIAN AIRPORTS ľ A SHORT ANALYSIS
ICAS2018-P9.2: Y. Eun, Korea Aerospace Research Institute, South Korea
AIRPORT SURFACE TRAFFIC SCHEDULING WITH CONSIDERATION OF DE-ICING OPERATIONS
ICAS2018-P9.3: Jie REN╣, LIli WANG╣; ╣Civil Aviation University of China, China
VISUAL FLIGHT PROCEDURE DESIGN IN CHINA
ICAS2018-P9.4: B Cui╣, L Meilong╣, R Curran, Delft University of Technology, Netherlands; ╣Nanjing University of Aeronautics and Astronautics, China
CASCADING FAILURE OF NODES AND THEIR LINKS IN A COMPLEX NETWORK
ICAS2018-P9.5: R. Fusaro, Politecnico di Torino, Italy
SELECTION OF OPTIMAL RE-PLANNING STRATEGY FOR FLEET OF UAVS IN NOMINAL AND EMERGENCY MONITORING SCENARIOS
ICAS2018-P9.6: L. F. Enoch, UNIVERSIDADE FUMEC, Brazil
THE LOW-COST LOW-FARE MODEL IN THE BRAZILIAN AVIATION MARKET: ECONOMIC CONTRIBUTIONS

10 - Safety and Security

ICAS2018-P10.1: P. -R. Alves, ANAC, Brazil
DISCUSSION ON UMANNED AIRCRAFT AUTOMATIC FLIGHT CONTROL SYSTEM AIRWORTHINESS CERTIFICATION
ICAS2018-P10.2: H. Inokuchi, Japan Aerospace Exploration Agency, Japan
FLIGHT DEMONSTRATION OF A LONG RANGE ONBOARD DOPPLER LIDAR
ICAS2018-P10.3: Lukas H÷hndorf╣, Chong Wang╣, Phillip Koppitz╣, Sebastian Wei▀╣, Sergio Olmos, Evelop Airlines, Spain; Claudia Czado, Technical University of Munich, Mathematical Statistics, Germany; Florian Holzapfel╣; ╣Technical University of Munich, Flight System Dynamics, Germany
INTEGRATION OF VINE COPULA DEPENDENCE STRUCTURES INTO SUBSET SIMULATION FOR ACCIDENT PROBABILITY QUANTIFICATIONS
ICAS2018-P10.4: Chong Wang╣, Florian Holzapfel╣; ╣Technical University of Munich, Germany
EVALUATION OF AIRCRAFT BRAKING PERFORMANCE BASED ON OPERATIONAL FLIGHT DATA
ICAS2018-P10.5: P. M. Razaboni, Embraer SA, Brazil
UNIVERSAL DESIGN FOR AIRCRAFT SAFETY
ICAS2018-P10.6: G. C. Rocha, Konatus, Brazil; J. Alfredson, Saab, Sweden; L. G. Trabasso╣, A. N. Almeida╣, A. C. Matheus╣, D. H. Arjoni╣, M. A. R. Diaz╣; ╣ITA, Brazil
A ROADMAP FOR ASSESSING HUMAN FACTORS INFLUENCE ON PILOT PERFORMANCE BASED ON SIMULATED FLIGHTS
ICAS2018-P10.7: E. Fouladi, Sharif University of Engineering (SUT), Iran
CLASSIFICATION OF MATURE AND NEW INSPECTION AND MONITORING TECHNOLOGIES USED IN AGING AIRCRAFT LIFE EXTENSION

11 - Operations and Sustainment

ICAS2018-P11.1: Song Guibin Guibin, Aircraft Strength Research Institute of China, China
ANALYSIS AND PARAMETER INFLUENCE OF COMPOSITE LAMINATES WITH WEDGE-SHAPED SCARF PATCH REPAIR
ICAS2018-P11.2: M. C. C. Ara˙jo, Instituto Tecnolˇgico da Aeronßutica (ITA), Brazil; M. L. C. C. Reis, Instituto de Aeronßutica e Espašo (IAE), Brazil; P. A. S. Alves, Universidade de TaubatÚ, Brazil
MAINTENANCE PLAN EVOLUTION PROCESS BASED ON FIELD DATA EXPIRIENCE
ICAS2018-P11.3: R. B. Parra╣, J. Laguardia╣; ╣FUMEC University, Brazil
ERRORS FROM ENGINEERING IN FLIGHT SAFETY
ICAS2018-P11.4: E. Fouladi, Sharif University of Engineering (SUT), Iran
RELIABILITY ASSESSMENT OF AGING AIRCRAFT STRUCTURES UNDER CORROSION FATIGUE BASED ON FORM METHOD
ICAS2018-P11.5: Gangde LU╣, TianXiong WU╣; ╣Chengdu Aircraft Design & Institute, China
THE TECHNIQUE AND MODELLING FOR EQUIPMENT MAINTAINABILITY QUANTIFICATION IN 3D DIGITAL AIRCRAFT DESIGN CONDITION
ICAS2018-P11.6: R. B. Parra, Fumec University , Brazil; J. C. Almeida Jr, Fumec University, Brazil
AIRCRAFT MAINTENANCE PROCEDURE MODELS
ICAS2018-P11.7: L. I. ABREU, ITA, Brazil
TAKE-OFF AND LANDING AIRCRAFT NOISE: AN ASSESSMENT BASED ON TRAJECTORY SEGMENTATION
ICAS2018-P11.8: B.S.C, E.G.C, J. Camba, Universidade Federal de Minas Gerais, Brazil
SIMULATION AND OPTIMIZATION OF THE TAIL ASSIGNMENT AND MAINTENANCE PLANNING PROBLEMS

12 - Host nation

ICAS2018-P12.1: R B Parra, FUMEC University, Brazil
LEONARDO DA VINCI┤S INTERDISCIPLINARITY