ACCEPTED PAPERS - CATEGORY C - INTERACTIVE PRESENTATIONSThese papers will be presented in the Interactive Presentations area |
1.1 - Aircraft Design and Integrated System (Basics and Theory) |
|
ICAS2024_1046: J.L.C. Chan¹, Y. Sun¹, H. Smith, Cranfield University , United Kingdom; ¹Cranfield University, United Kingdom PERFORMANCE ENHANCEMENTS BETWEEN DIFFERENT APPLICATIONS OF ALTERNATIVE FUELS AND NOVEL AIRCRAFT CONFIGURATIONS |
|
ICAS2024_0068: S. Hosseini¹, M.A. Vaziry Zanjany¹, H.R. Ovesy¹, E. Lekzian, Semnan University, Iran; ¹Amirkabir University of Technology, Iran APPLICATION OF LAMBDA FRAMEWORK FOR AIRCRAFT MULTIDISCIPLINARY DESIGN, ANALYSIS AND OPTIMIZATION |
|
ICAS2024_0744: B.T.V. Carnielo¹, D.D. Bueno¹; ¹São Paulo State University, Brazil THE INFLUENCE OF DIFFERENT WING MOTIONS ON THE LIFT IN BIO-INSPIRED AERIAL VEHICLES |
|
ICAS2024_1036: J.Z. Li¹, Y.J. Yang¹, Y.F. Zhang¹; ¹School of Aerospace Engineering, Tsinghua University, China AIRFOIL PRESSURE PREDICTION BASED ON PHYSICS-INFORMED DEEP LEARNING APPROACH |
|
ICAS2024_0042: L. Paletti¹, L. Boggero¹, G. Wende¹, B. Nagel¹; ¹German Aerospace Center (DLR), Germany TRANSLATING THE CONCEPT OF SUSTAINABILITY FOR THE DETERMINATION OF REQUIREMENTS FOR THE DESIGN OF FUTURE AIRCRAFT |
|
ICAS2024_0575: M. Alberti¹, G. Apuleo¹, A. Calia¹, D. Cirio¹, A. Cozzolino¹, F. Gravano¹, M. Mancini¹, F. Nunciato¹, A. Terrile¹; ¹Piaggio Aerospace, Italy AICRAFT-0 SAT D1 FOR GREENER, SAFER AND AFFORDABLE MORE ELECTRIC (MEA) AND FLY-BY-WIRE (FBW) SMALL AIR TRANSPORT (SAT) |
1.2 - Aircraft Design and Integrated System (Applications) |
|
ICAS2024_1021: I. Kopec¹, D. Matyja¹; ¹Polish Air Force University, Poland DESIGN OF REMOTE-CONTROLLED GROUND BASED AIRCRAFT TUG |
2 - Systems Engineering and Integration |
|
ICAS2024_0550: X. Li¹, L. Deng¹, Y. Ge¹, Y. Pei¹, Y. Gu², L. Cao², A. Shi¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China; ²Shanghai Electro-Mechanical Engineering Institute, China RESEARCH ON ROUTE PLANNING METHOD FOR UAV SWARM AREA COVERAGE MISSIONS BASED ON COMPLEX NETWORKS |
|
ICAS2024_0962: Y.-Z. Wang¹, B.-L. Shang¹, P.-F. Li¹, W.-Z. Liu¹, R.-X. Lin¹, K.-A. Xing¹, Y.-T. Deng¹; ¹School of Aeronautics, Northwestern Polytechnical University, China EFFECTIVENESS EVALUATION METHOD FOR AVIATION EMERGENCY RESCUE SYSTEM OF SYSTEMS BASED ON EFFECT CHAIN |
|
ICAS2024_0603: C. Mirabella¹, M. Tuccillo¹, P. Della Vecchia¹; ¹Università degli Studi Federico II, Italy A MODEL BASED SYSTEM ENGINEERING APPROACH TOWARDS AIRCRAFT DIGITAL CERTIFICATION |
|
ICAS2024_0148: B. Boden¹, M. Padilha¹, T. Burschyk¹, C. Cabaleiro de la Hoz¹, E. Moerland¹, M. Fioriti, Politecnico di Torino, Germany; ¹DLR, Germany AUTOMATING THE VERIFICATION OF GEOMETRIC REQUIREMENTS FOR AIRCRAFT FUEL SYSTEMS USING KNOWLEDGE-BASED ENGINEERING |
|
ICAS2024_0211: W. Cheng¹, R. Fan, Aviation Industry Corporation of China, Ltd (AVIC), China; J. Xu¹, H. Zhang¹, Z. Wang¹; ¹Aviation Industry Development Research Center of China (ADR), China RESEARCH ON TECHNOLOGICAL INNOVATION CAPABILITY EVALUATION INDEX FOR AVIATION INDUSTRIES |
|
ICAS2024_0843: Z. Cui¹, M. Luo¹, J. Lu¹, J. Wang¹; ¹Beihang University, China A SEMANTIC MODEL-BASED SYSTEMS ENGINEERING APPROACH FOR SUPERSONIC BUSINESS JET CONCEPTUAL DESIGN |
3.1 - Aerodynamics – CFD Methods and Validation |
|
ICAS2024_0205: Q. Nguyen Dinh¹, H. Tran The¹, G. Sharma², J. Tanimoto²; ¹Le Quy Don Technical University, Vietnam; ²Kyushu University, Japan APPLICATION OF ARTIFICIAL NEURAL NETWORK (ANN) FOR PREDICTION OF DRAG COEFFICIENT OF AXISYMMETRIC BOATTAIL MODELS |
|
ICAS2024_0311: B. Guo¹, Y.F. Lu¹, B. Wang, Chinese Academy of Military Science, China; Z. Guo¹, G.W. Jia¹, D.N. Liu¹; ¹National University of Defense Technology, China SEPARATION SAFETY ANALYSIS IN VARIABLE LAUNCH CONDITION OF SMALL AIR-LAUNCHED UAVS BASED ON NUMERICAL SIMULATION AND FLIGHT TEST |
|
ICAS2024_0104: M. Turner¹, J. Sharpe¹, M. Kopacz¹, D. Standingford¹, C. Sequeira², B. Sanby², C. Rider²; ¹Zenotech, United Kingdom; ²Flare Bright, United Kingdom VALIDATION OF CFD-BASED DATA SERVICE FOR DRONE INSPECTION OF WIND FARMS WITH FLIGHT TEST DATA |
|
ICAS2024_0531: M. Jian¹, Y. Xiao¹, X. Cheng¹, W. Dong¹; ¹Shanghai Jiao Tong University, China CONJUGATED HEAT TRANSFER SIMULATION OF BUOYANCY-INDUCED FLOW AND HEAT TRANSFER MECHANISMS IN A COMPRESSOR CAVITY |
|
ICAS2024_0197: G. Sharma¹, T.H. Tran, Le Quy Don Technical University, Vietnam; J. Tanimoto¹; ¹Kyushu University, Japan APPLICATION OF CONVOLUTIONAL NEURAL NETWORKS IN DETERMINING THE VELOCITY AND PRESSURE FIELDS AROUND AIRFOIL MODELS |
|
ICAS2024_1084: J. Parez¹, P. Kovar¹, T. Vampola¹; ¹Czech Technical University in Prague, Czech Republic PREDICTION OF TRANSIENT DEFORMATION BY COUPLING CFD AND FEM ANALYSIS USING MACHINE LEARNING BASED CORRELATION FUNCTION |
|
ICAS2024_0791: J.L. Kurniawan¹, M. Hu¹; ¹Institut Teknologi Bandung, Indonesia SURROGATE MODELING OF VORTEX SHEDDING TURBINE IN LOW REYNOLDS NUMBER |
|
ICAS2024_0952: F. Duan¹, J.-Y. Li¹, Z.-D. Li, Aerospace Life-support Industries Ltd, China; M.-B. Tong¹; ¹Nanjing University of Aeronautics and Astronautics, China RESEARCH ON AERODYNAMIC PERFORMANCE OF OVERSIZE MODULAR PARAFOIL IN RANDOM WIND FIELD |
|
ICAS2024_0704: L.-Y. Huang¹, X. Zhao¹, X.-C. Li, Nanjing University of Aeronautics and Astronautics, China; ¹School of Aeronautics, Northwestern Polytechnical University, Xi, China ANALYSIS OF AERODYNAMIC INTERFERENCE CHARACTERISTICS AND AEROACOUSTICS FOR HIGH-SPEED COMPOSITE HELICOPTER IN HOVER |
|
ICAS2024_1033: M. Nemati¹, A. Jahangirian¹; ¹amirkabir university of technology, Iran MACHINE LEARNING INTEGRATION IN COMPUTATIONAL FLUID DYNAMICS FOR RAPID FLOW FIELD PREDICTION |
|
ICAS2024_0035: H. Qiao¹, F. Qin¹, S. Deng¹; ¹Nanjing University of Aeronautics and Astronautics, China A NUMERICAL VIRTUAL FLIGHT PLATFORM DEVELOPMENT AND ITS APPLICATION ON HIGH MANEUVERABILITY FLIGHT VEHICLES |
3.2 - Experimental Aerodynamics |
|
ICAS2024_0219: R. Bardera¹, A.A. Rodríguez-Sevillano², J.C. Matías¹, E. Barroso¹, M. Ojeda², J. Fernández²; ¹Instituto Nacional de Técnica Aeroespacial (INTA)., Spain; ²Escuela Técnica Superior de ingeniería Aeronáutica y del Espacio, Spain EXPLORING WINGTIP COLUMNAR VORTEX GENERATORS FOR UAV PERFORMANCE ENHANCEMENT |
|
ICAS2024_0218: D. Damljanovic¹, D. Vukovic¹, L. Petrovic¹; ¹Military Technical Institute, Serbia REVITALIZATION OF A FLOW-CELL DEVICE FOR AIR INTAKE TESTING AND ITS INTEGRATION WITH WIND TUNNEL SYSTEMS |
|
ICAS2024_0526: Y.-F. Wang¹, B.-F. Song¹, Y. Luo¹, X.-Y. Lang¹, W. Wang¹; ¹Northwestern Polytechnical University, China INFLUENCE OF REINFORCED TRAILING EDGE ON FLAPPING WING AERODYNAMIC FORCE AND DEFORMATION |
3.3 - Basic Fluid Dynamics and Flow Control |
|
ICAS2024_0817: Y. Xu¹, Y.-G. lLyu¹, J.-P. Hu¹, Z. Liu¹; ¹Northwestern Polytechnical University, China EXPERIMENTAL STUDY ON MULTI-ATTITUDE OIL SUPPLY STRUCTURE |
|
ICAS2024_0426: S.-T. Peng¹, F.-Z. Chen¹, H. Yan¹, X.-Q. Sun¹; ¹Northwestern Polytechnical University, China NUMERICAL INVESTIGATION ON THE EFFECT OF REYNOLDS NUMBER ON TANDEM DROPLET |
3.4 - Applied Aerodynamics |
|
ICAS2024_0690: K.-Y. Zhou¹, S.-Q. Zhang, Jilin Chongtong Chengfei New Material Co., LTD, China; W.-P. Song¹, J.-H. Xu¹, Z.-H. Han¹; ¹Northwestern Polytechnical University, China RESEARCH ON MULTI-OBJECTIVE AERODYNAMIC/STRUCTURAL DESIGN OPTIMIZATION METHOD FOR LARGE THICKNESS FLATBACK AIRFOILS |
|
ICAS2024_0639: C. Wei¹, C. Rao¹, L. Yang¹, T. Zhang¹; ¹Aerodynamics Research Institute, China AERO-KINEMATIC OPTIMIZATION OF HIGH-LIFT DEVICES WITH DOWNWARD DEFLECTION OF SPOILER |
|
ICAS2024_0449: Y. Li¹, X. Xu¹, Z. Zhou¹, Y. Bai¹, H. Wang¹, B. Xu¹; ¹Northwestern Polytechnical University, China SIMULATION STUDY ON AERODYNAMIC CHARACTERISTICS OF COMBINED LOW ASPECT RATIO UAV |
|
ICAS2024_0158: R.H. Morais¹, L.F. Ferreira Marques, ISEC, Portugal; A. Resende Rodrigues da Silva¹, R. Melicio, LAETA-IDMEC, Instituto Superior Técnico, Universidade de Lisboa, Portugal; ¹LAETA-AEROG, Universidade da Beira Interior, Portugal MODELLING ASTEROID TRAJECTORY IN EARTH’S ATMOSPHERE |
|
ICAS2024_0473: J. Liu¹, D. Xue¹; ¹School of Aeronautics, Northwestern Polytechnical University, China RESEARCH ON OPTIMAL TORSIONAL DEFORMATION OF FLAPPING WING |
|
ICAS2024_0265: M. Nayman¹, R.E. Perez¹; ¹Royal Military College of Canada, Canada LOCALIZED AERODYNAMIC SHAPE OPTIMIZATION FOR AUTOMOTIVE APPLICATIONS |
|
ICAS2024_0665: D. Guagliardo¹, E. Cestino¹, A. Virdis¹, A. Alfero¹, V. Sapienza¹; ¹Politecnico of Turin, Italy NUMERICAL-THEORETICAL EVALUATION OF THE DITCHING OF A HULL WITH DIHEDRAL ANGLES BETWEEN -5 AND 20 DEGREES |
|
ICAS2024_0551: Z. Xu¹, D. Li¹, J. Cai¹, J. Han, N, China; ¹Northwestern Polytechnical University School of Aeronautics, China LONG-WAVE INSTABILITY OF AIRCRAFT WAKE VORTEX UNDER SHEAR CROSSWIND |
4.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance |
|
ICAS2024_0933: D.-B. Li, China; H.-X. Huang, China; X.-C. Liu, China; P.-Y. Hou, China; H.-H. Liao, China A METHOD FOR OPTIMISING THE ARRANGEMENT OF INTERNAL CHANNELS IN AIRCRAFT HYDRAULIC MANIFOLDS MANUFACTURED BY ADDITIVE MANUFACTURING |
|
ICAS2024_0806: M. Mucha¹, D. Sikorski, 41st Training Air Base, Poland; R. Szczepaniak¹, R. Babel¹, A. Krzyzak¹, T. Zahorski¹; ¹Polish Air Force University, Poland EFFECT OF INFILL STYLE AND DENSITY ON SELECTED MECHANICAL PROPERTIES OF THE CARBON FIBRE REINFORCED ABS MFD FILAMENT |
|
ICAS2024_0525: E.G. Park, South Korea; S.H. Jeong, South Korea; J.Y. Cho, South Korea; J.H. Kim, South Korea DEVELOPMENT OF A MACHINE LEARNING-BASED STRESS SPECTRUM ESTIMATION TECHNIQUE FOR FATIGUE MONITORING |
|
ICAS2024_0422: H. Peng¹, B. Wang¹, Y. Zhang¹, L. Ji¹, S. Li¹; ¹AVIC the First Aircraft Institute, China STUDY ON FATIGUE PROPERTIES OF TITANIUM ALLOY BASE MATERIAL AND WELDED STRUCTURE IN THERMAL COMBINED ENVIRONMENT |
|
ICAS2024_0275: R. Szczepaniak¹, P. Przybylek¹, D. Szczechula¹, A. Krzyzak¹, A. Komorek¹, G. Woroniak, Bialystok University of Technology, Poland; ¹Polish Air Force University, Poland ANALYSIS OF THE POSSIBILITY OF INCREASING THE THERMAL RESISTANCE OF EPOXY RESIN WITH CWNT AND MMT |
|
ICAS2024_0368: Y. Liu¹, W. Wang¹, J. Zhao¹, Y. Song¹, L. Zou¹; ¹Chongqing University, China WEAR EVOLUTION OF PYRAMID-STRUCTURED ABRASIVE BELTS AND ITS EFFECT ON GRINDING OPERATIONS |
|
ICAS2024_0316: W. Stryczniewicz¹, T. Kwiatkowski¹, I. Kaminska², M. Chojnacki², K. Fronc²; ¹?ukasiewicz Research Network - Institute of Aviation, Poland; ²Institute of Physics Polish Academy of Sciences, Poland THERMAL HISTORY PAINT UNDER HIGH SUBSONIC FLOW |
|
ICAS2024_0739: P.E. Boffa¹, E. Casciaro¹, P. Bettini¹; ¹Politecnico di Milano, Italy FULLY-EMBEDDED PRESSURE SENSOR FOR AERODYNAMICS SURFACES BASED ON FBG TECHNOLOGY |
4.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity |
|
ICAS2024_1015: S.-Y. Sun¹, H.-Z. Wang¹, R. Yang¹, W. Qian¹; ¹Dalian University of Technology, China MODELING AND VALIDATION OF MORPHING WING TRAILING EDGE BASED ON ZERO POISSON'S RATIO HONEYCOMB |
|
ICAS2024_0530: R. Hou¹, B.T. Wang, Department of Strength Design, The First Aircraft Institute of A, China; Z.X. Zhu¹, W.C. Gao¹; ¹Department of Astronautical Science and Mechanics, HIT, China EXPERIMENTAL INVESTIGATION AND NUMERICAL ANALYSIS OF THE EFFECT OF TEMPERATURE ON THE MECHANICAL PROPERTIES OF AEROSPACE COMPOSITE-METAL HYBRID JOINTS |
|
ICAS2024_0445: Y. Zhang¹, H. Zhan¹, B. Mi¹, M. Zhang¹; ¹Northwestern Polytechnical University, China INVESTIGATION ON INFLUENCE PARAMETER OF AIRCRAFT-MISSILE SEPARATION BY CONSIDERING AEROELASTICITY |
|
ICAS2024_0072: Z. Guo¹, A. Tang¹, Q. Jing¹; ¹Chinese Flight Test Estsblishment, China FLIGHT LOADS RESEARCH OF TWIN VERTICAL TAIL FOR BLENDED WING-BODY AIRCRAFT BASED ON STRAIN GAUGE CAILBRATION |
5 - Propulsion |
|
ICAS2024_0865: M. Zhang¹, J. Jiao¹, J. Zhang¹, Z. Zhang¹; ¹Chinese Academy of Sciences, China LOW ENERGY CONSUMPTION DESIGN METHOD AND STRATEGY FOR HIGH-ALTITUDE PROPELLERS BASED ON FLIGHT PROFILE |
6.1 - Flight Dynamics and Control (Control & Modelling) |
|
ICAS2024_0805: S. Kolb, CREA, France PILOT INDUCED OSCILLATIONS AND FLIGHT PHASES IDENTIFICATION OF THE SPACE SHUTTLE AND TRANSPORT AIRPLANES |
|
ICAS2024_0828: M. Shin¹, M.-J. Tahk¹, B. Kim¹, C.-H. Lee¹; ¹Korea Advanced Institute of Science and Technology, South Korea PURSUIT-BASED LONG-RANGE AIR-TO-AIR MISSILE MIDCOURSE GUIDANCE ROBUST TO CHANGES IN THE PREDICTED IMPACT POINT |
|
ICAS2024_0491: M. Naruoka¹, T. Ninomiya¹; ¹Japan Aerospace Exploration Agency, Japan DATA ORIENTED EVALUATION OF FLIGHT CHARACTERISTIC MODELS BY USING BAYES FACTOR |
|
ICAS2024_1182: C. Döll¹, S. Waitman¹; ¹ONERA, France CONTROL ALLOCATION FOR A DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT USING DIFFERENTIAL THRUST |
|
ICAS2024_0627: M.-W. Kang¹, D.-W. Lee², S.-H. Yun¹, H.-C. Bang²; ¹ADD, South Korea; ²KAIST, South Korea DATA-DRIVEN MODEL DISCOVERY AND CONTROL OF HIGH-PERFORMANCE TRAINER AIRCRAFT VIA SPARSE IDENTIFICATION OF NONLINEAR DYNAMICS |
|
ICAS2024_1119: C.R. Li¹, W.Q. Li¹, Y. Li¹, S. Tang¹; ¹Northwestern Polytechnical University, China A NOLINEAR MODEL PREDICTIVE CONTROL METHOD FOR AIRBREATHING HYPERSONIC VEHICLE BASED ON KOOPMAN OPERATOR |
|
ICAS2024_0977: Y. Liu¹, Y.-H. Nong², X. Liu, Shanghai Aircraft Airworthiness Certification Center, China; Z.-H. Cheng², M.-X. Zhang¹; ¹Northwestern Polytechnical University, China; ²AVIC General Huanan Aircraft Industry, China MODELING AND FLIGHT CONTROL LAW DESIGN FOR A SEAPLANE DURING WATER SURFACE TAKEOFF |
|
ICAS2024_1070: Z.-F. Luo¹, Y.-J. Lian, National University of Defense Technology, China; C. Zhang, Chinese Academy of Sciences, China; T. Zhang¹; ¹Sun Yat-sen University, China TRAJECTORY DESIGN FOR ASTEROID SAMPLE RETURN COMBINING BALLISTIC CAPTURE AND AEROBRAKING |
|
ICAS2024_0621: C. Zhai¹, B. Song¹, Q. Fu¹, J. Xuan¹, J. Li¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China DYNAMICS ANALYSIS AND CONTROL OF A LARGE WINGSPAN FLAPPING-WING VEHICLE |
|
ICAS2024_0938: R.K. Nangia¹, T. Nangia¹; ¹Nangia, United Kingdom GROUND EFFECT ON A SLENDER 65º DELTA WING WITH SIDESLIP, IMAGE METHOD, USING EULER |
|
ICAS2024_1115: C. Varriale¹, F. Yunus¹, M. Snellen¹; ¹Delft University of Technology, Netherlands OPTIMAL APPROACH AND DEPARTURE TRAJECTORIES WITH ACOUSTIC FOOTPRINT ASSESSMENT FOR AN AIR MOBILITY QUAD-ROTOR |
|
ICAS2024_0223: K.H. Kienitz, Instituto Tecnologico de Aeronautica, Brazil; A. Gonzalez Sorribes¹, R. Sanz Diaz¹, C. Braga de Mendonça, Boeing Brasil, Brazil; P.J. Garcia¹; ¹Universitat Politecnica de Valencia, Spain STRUCTURED H-INFINITY DESIGN OF PREDICTORS FOR THE MONITORING OF AN AIRCRAFT IN ITS FLIGHT ENVELOPE |
|
ICAS2024_0494: C. Santoro¹, S.R. Bassolillo, University of Naples Parthenope, Italy; A. Ferraro, University of Reggio Calabria Mediterranea, Italy; L. Blasi¹, I. Notaro¹; ¹University of Campania L. Vanvitelli, Italy A MODEL PREDICTIVE CONTROL ALGORITHM FOR THE FORMATION CONTROL OF NANOSATELLITES IN LEO ORBIT |
6.2 - Flight Dynamics and Control (UAV related) |
|
ICAS2024_0535: J.L. Kurniawan¹, P.B.A. Baylon¹, R.A. Sasongko¹; ¹Institut Teknologi Bandung, Indonesia A NOVEL APPROACH TO AUTOMATED TRACKING CONTROL OF HYBRID TILTING ROTOR UAVS USING LQG CONTROLLER AND STATE MACHINE |
|
ICAS2024_0231: H. Shi¹, S. Li, AVIC Chengdu Aircraft Industrial (Group) Co., Ltd., China; Z. Huang¹, S. Li¹, A. Li¹, Y. Zhou¹; ¹BEIHANG UNIVERSITY, China MANNED AND UNMANNED AERIAL VEHICLES COOPERATIVE COMBAT FRAMEWORK BASED ON LARGE LANGUAGE MODELS |
|
ICAS2024_1209: A. Bagherzadeh¹, F. Saghafi¹; ¹Sharif University of Technology, Iran AN OPTICAL FLOW BASED GUIDANCE ALGORITHM FOR A QUADROTOR UAV MOVING INSIDE CIRCULAR CORRIDORS |
|
ICAS2024_0578: L. Wang¹, X. Yang¹, Y. Luo¹, H. Chen¹, J. Li¹; ¹NORTHWESTERN POLYTECHNICAL UNIVERSITY, China DESIGN OF ATTITUDE CONTROL SYSTEM FOR DRAGONFLY-INSPIRED FLAPPING WING AERIAL VEHICLE |
|
ICAS2024_0664: D. Kim¹, H.J. Kim¹; ¹Seoul National University, South Korea AUTONOMOUS LANDING OF A QUADROTOR ON A MOVING TARGET WITH OCCLUSION AVOIDANCE MANEUVER |
|
ICAS2024_0972: H.-X. Huang¹, D.-B. Li¹, P.-Y. Qi¹, Y.-X. Shang¹; ¹beihang university, China ULTRA-LOW-ALTITUDE PENETRATION PATH PLANNING FOR FIXED-WING AIRCRAFT BASED ON NMP ALGORITHM |
7 - Systems, Subsystems and Equipment |
|
ICAS2024_0123: R. Tirschmann¹, D. Metzler², T. Koch², M. Spieler¹, W. Nendel¹, L. Kroll¹; ¹Technische Universität Chemnitz, Germany; ²Liebherr-Aerospace Lindenberg GmbH, Germany SIMULATION AND VERIFICATION OF HYDRAULIC ROTOR GAP PARAMETERS OF A NOVEL HIGH EFFICIENT WET ELECTRO MOTOR PUMP FOR AEROSPACE APPLICATIONS |
|
ICAS2024_0755: C.C.D. Silva¹, Y. Castro¹, A. Sarmento¹, E. Villani¹; ¹ Instituto Tecnológico de Aeronáutica, Brazil MULTIPLATFORM SIMULATION USING ROS |
|
ICAS2024_0033: G.-M. Li¹, W.-T. Xie¹; ¹AVIC XI’AN Aeronautics Computing Technique Research Institute, China THE DESIGN FOR TESTABILITY OF CIVIL AIRCRAFT AVIONICS SYSTEMS |
|
ICAS2024_0731: Q.-H. Nghiem¹, T.-G. Nguyen¹, B.-M. Pham¹, P.-M. Nguyen¹; ¹Viettel Aerospace Institute, Vietnam AERODYNAMIC DESIGN METHODOLOGY OF A NON-UNIFORM PERFORATED INVERSE CONICAL FLOW SPREADER IN INTERMITTENT BLOW DOWN WIND TUNNEL |
|
ICAS2024_1043: C. Jiang¹, Y. Shang¹, T. Yu¹, Z. Liu¹, M. Li¹; ¹Beihang University, China MODELING AND ANALYSIS OF ELECTRO-HYDROSTATIC ACTUATORS EFFICIENCY |
|
ICAS2024_0674: X. Hu¹, Y. Fu¹, D. Lyu¹, M. Sun¹, S. Zhao, Beijing Institute of Precision Mechatronics and Controls, Labora, China; J. Fu¹, J. Zhao¹; ¹School of Mechanical Engineering and Automation, Beihang Univers, China RESEARCH ON MODELING THE TEMPERATURE FIELD OF A NEW AEROSPACE SERVO ELECTRO-HYDROSTATIC MODULE BASED ON THERMO-MAGNETIC BIDIRECTIONAL COUPLING ANALYSIS |
|
ICAS2024_0866: Y. Ding¹, D. Xu¹, Y. Li¹, Z. Fang¹, T. Chen¹, H. Zhang, Airforce Engineering University, China; B. Chen, Shanghai University, China; ¹Aviation Industry of China (AVIC), China ATTITUDE ESTIMATION USING KALMAN FILTERING FOR SPACEBORNE SAR SYSTEMS |
|
ICAS2024_0511: S. Wehrend¹, K. Zumach¹, L. Schwan¹, D. Krause¹; ¹Hamburg University of Technology (TUHH), Germany TOWARDS A HOLISTIC APPROACH TO INCREASE SUSTAINABILITY IN AIRCRAFT CABIN DESIGN |
|
ICAS2024_0504: R. Fallucca¹, A. Iannuzzo¹, S. Gallina¹, E. Cestino¹, V. Sapienza, Aeronautical Engineering Consultant, Italy; ¹Politecnico di Torino, Italy EXPERIMENTAL RESULTS OF ANTENNA PLACEMENT TEST ON A CARBON-FIBER SCALE REPLICA OF THE S55X SEAPLANE |
|
ICAS2024_0697: Y. Zhang¹, Y. Yang², Q. Xiao², R. Li¹, Z. Xu¹; ¹Northwestern polytechnical University, China; ²China Academy of Launch Vehicle Technology, China AN IMPROVED END-TO-END STAR MAP RECOGNITION METHOD FOR AEROSPACE VEHICLE |
|
ICAS2024_0194: H.-C. Ma¹, T. Guo¹, G.-D. Li¹, J.-B. Bai¹; ¹Aviation Industry Corporation of China-The First Aircraft INST, China CONFIGURATION ANALYSIS OF INTEGRATED THERMAL MANAGEMENT BASED ON THE TURBINE-FAN REFRIGERATION SYSTEM |
10 - Safety and Security |
|
ICAS2024_1186: T.-J. Jiang¹, Z.-P. Luo¹, Z. Kan¹, J.-W. Xiang¹, X.-C. Liu², C.-Y. Bai², X.-L. Xi²; ¹Beihang University, China; ²Aircraft Strength Research Institute, China IMPROVING DISTRIBUTION OF CRASH ENERGY ABSORPTION FOR CIVIL AIRCRAFT BASED ON PROGRESSIVE BENDING FAILURE MECHANISM |
|
ICAS2024_0587: G. Li¹, Y.-D. Teng¹, Z.-L. Wang¹, T.-G. Xu¹, S.-T. Ding, Civil Aviation University of China,, China; ¹Beihang University, China A METHOD FOR AUTOMATIC GENERATING SAFETY ANALYSIS BASED ON AVIATION PISTON ENGINE MODEL |
11 - Operations and Sustainment |
|
ICAS2024_0165: M.C. Berschik¹, S. Wehrend¹, F.N. Laukotka¹, D. Krause¹; ¹Hamburg University of Technology, Germany DIGITALISATION AND SUSTAINABILITY IN CABIN DESIGN: SYNERGIES AND DEPENDENCIES |
|
ICAS2024_0065: D.Y. Sabag¹, O. Yakimenko, Naval Postgraduate School, United States; H. Alian¹; ¹Israeli Air Force, Israel DIGITAL TWIN OF AN AIRCRAFT LANDING GEAR TO ENHANCE FAILURE ANALYSIS AND MANAGE PREDICTIVE MAINTENANCE |
|
ICAS2024_0545: S. Wildermuth¹, W. Veraburenon¹, T. Bellier¹, C. Bil¹; ¹RMIT University, Australia LIFE CYCLE ASSESSMENT OF ALTERNATIVE LAUNCH METHODS |
|
ICAS2024_0350: E. Stefana¹, E. De Paola¹, L. Pustina¹, R. Patriarca¹, F. Mastroddi¹; ¹Sapienza University of Rome, Italy ENSURING THE NEXT GENERATION GREEN AIRCRAFT’ SUSTAINABILITY FROM THE DESIGN PHASE VIA A LIFE-CYCLE COST ANALYSIS |
14 - Education and Training |
|
ICAS2024_1098: G. Kontos¹, O. Lehmann¹; ¹Abu Dhabi University, United Arab Emirates DESIGNING A FRAMEWORK FOR FLIGHT SIMULATOR TRAINING SCENARIOS. AN EVIDENCE BASED TRAINING APPROACH. |