ACCEPTED PAPERS - CATEGORY C - INTERACTIVE PRESENTATIONThese papers were presented in the Interactive Presentations area |
1 - Aircraft Design and Integrated Systems |
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ICAS2020_0155: W. Wang, School of Aeronautics, Northwestern Polytechnical University, China; W. Yang¹, B. Song¹; ¹Research & Development Institute of NWPU, China NUMERICAL SIMULATION ON AERODYNAMIC CHARACTERISTICS OF BIONIC CORRUGATED FLAPPING WING |
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ICAS2020_1154: G.P. Qian¹, Y.H. Wang¹, C. Ma¹; ¹COMAC, China THE STUDY ON ANTI-ICING AREAS OF LEADING-EDGE SLATS IN MODERN CIVIL AIRCRAFT |
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ICAS2020_0317: J. Guo¹, Y. Li, School of Aeronautics, Northwestern Polytechnical University, China; M. Xu¹; ¹School of Astronautics, Northwestern Polytechnical University, China AN ADJOINT-BASDF AERO-STRUCTURAL DESIGN OPTIMIZATION METHOD USING DYNAMIC MESH TECHNOLOGY |
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ICAS2020_0154: D. Chen¹, Y. Li¹, Y. Li¹, L. Guan, Tsinghua University, China; Q. Wang, Beijing Aerospace Technology Institute, China; ¹Northwestern Polytechnical University, China CONCEPTUAL DESIGN OF A FIXED-WING AQUATIC UAV USING KNOWLEDGE BASED ENGINEERING |
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ICAS2020_0333: Y. Li¹, W. Yang ¹, A. Chen¹, R. Zhang¹; ¹School of Aeronautics, Northwestern Polytechnical University, China MECHANISM DESIGN AND AERODYNAMIC RESEARCH OF RETRACTABLE FOLDING FLAPPING WING |
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ICAS2020_0851: H.-L. Liu¹, M.-H. Tang¹, A.-Y. Zhu¹, W. Kong¹, H.-C. Shi, The First Military Representative Office of the Air Force Equipm, China; ¹Chengdu Aircraft Industrial (Group) Co., Ltd, China RESEARCH ON BARYCENTER MEASUREMENT METHOD IN LAUNCH OF ROCKET-BOOSTED UNMANNED AERIAL VEHICLES |
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ICAS2020_1155: C. Ma¹, Z.Y. Chen¹, C.H. Kong¹; ¹Shanghai Aircraft Design and Research Institute, China FAST ITERATIVE SIMULATION OF AIRLINER WING PLANFORM CONCEPTUAL DESIGN |
2 - Systems Engineering and Integration |
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ICAS2020_0744: S. Chang¹, D.W. Xia¹, Z.K. Yan¹, X. Jiang¹, J. Tang¹, H.T. Zhong¹; ¹COMAC, China SYSTEM ENGINEERING THINKING ON COMMERCIAL AIRCRAFT FLIGHT TEST |
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ICAS2020_0795: Q. Li¹, Y. An¹; ¹AVIC Xi'an Aircraft Industry Group Company LTD., China RESEARCH ON FUNCTIONAL HAZARD ASSESSMENT TECHNOLOGY OF MILITARY AIRCRAFT |
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ICAS2020_0581: Y. Guo¹, C. Ma¹, X. Dong¹; ¹Northwestern Polytechnical University, China RESEARCH ON SELECTION METHODS FOR AIRCRAFT LANDING GEAR SYSTEM HEALTH FEATURE PARAMETERS |
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ICAS2020_0077: W. Cheng¹, C. Xing¹, J. Xu¹, G. Song¹; ¹Aviation Industry Development Research Center of China , China RESEARCH ON ARCHITECTURE FRAMEWORK MODEL BASED EVALUATION INDEX FOR AVIATION SCIENCE & TECHNOLOGY MANAGEMENT |
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ICAS2020_1244: B. Wu¹, X.D. Qui¹; ¹NUAA, COMAC SADRI, China THE CIVIL AIRCRAFT DEVELOPMENT PROJECT RISK MANAGEMENT RESEARCH |
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ICAS2020_0168: L. Liu¹, X.F. Yang¹, G.M. Xiao¹, Q. Li, School of Mechanical Engineering, Shanghai Jiao Tong University, China; D. Wei¹, W. Tang, Southwest University of Science and Technology, China; ¹State Key Laboratory of Aerodynamics, CARDC, China AN ENERGY BASED WEIGHT ESTIMATION TECHNIQUE OF TWO-STAGE-TO-ORBIT REUSABLE LAUNCH VEHICLES |
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ICAS2020_0857: V.I. Budzko, FRC, Russia; A.V. Kan¹, G.G. Kazarinov¹, I.S. Mikhalyn ¹; ¹NRC Zhukovsky, Russia CREATING A MULTI-FUNCTIONAL EXPERT ANALYTICAL SYSTEM IN THE AIRCRAFT INDUSTRY AND THE FORMATION OF GENERAL REQUIREMENTS |
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ICAS2020_0720: Y.X. Che, Liaoning, China APPLICATION OF MBSE IN AERO-ENGINE STRUCTURAL PARAMETER CALCULATING SYSTEM |
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ICAS2020_1309: B. Xue, China; B. Luo, China; Z.J. Zhan, China; Y.H. Wang, China A NEW SERVICE-ORIENTED ARCHITECTURE DESIGN METHOD FOR AVIONICS SOS |
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ICAS2020_0252: W.Y. Cheng¹, C.G. Xing¹, G. Song¹; ¹Aviation Industry Development Research Center of China , China A CONTRASTIVE STUDY OF STANDARD SPECIFICATION FOR TECHNOLOGY READINESS ASSESSMENT |
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ICAS2020_0803: J. Shen¹, Q. Zhou¹, B.F. Li¹, C. Chen¹; ¹Chinese Aeronautical Radio and Electronics Research Institute, China CO-SIMULATION OF SYSML AND SIMULINK/MODELICA USING FMI |
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ICAS2020_0485: C.-J. He¹, L.-I. Wang¹, J.-H. Yang¹; ¹xi’an aircraft design institute, China COMPREHENSIVE REDUNDANCY MANAGEMENT AND VERIFICATION STRATEGY FOR TASK-BASED AIR MANAGEMENT SYSTEM |
3.1 - Aerodynamics – CFD Methods and Validation |
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ICAS2020_1106: W. Jin¹, S.E. Peng¹, J.M. Wu¹, J. Lei¹, W.T. Ji¹; ¹Xian Jiaotong University, China FLOW AND HEAT TRANSFER MECHANISM OF JET IMPINGEMENT COOLING ONTO MID-CHORD REGINE OF TWISTED BLADE |
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ICAS2020_1172: C. Tang¹, W.Q. Yang¹, B.F. Song¹, X.Y. Lang¹; ¹Northwestern Polytechnical University, China AERODYNAMIC ANALYSIS OF DRAGONFLY WINGS SPACE DISTRIBUTION ON THREE-DIMENSIONAL DURING HOVERING FLIGHT |
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ICAS2020_0315: H. Chen, China; X. Yuan, China; S. Meng, China; R. Hua, China; Z. Tang, China; L. Bi, China SIMULATION OF HIGH REYNOLDS NUMBER VISCOUS FLOW BASED ON ADAPTIVE CARTESIAN GRID |
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ICAS2020_1167: Z.C. Zhu¹, B.F. Song¹, W.Q. Yang¹, X.Y. Lang¹; ¹Northwestern Polytechnical University, China NUMERICAL SIMULATION OF SWEEPING MOTION EFFECTS ON THE HOVERING DRAGONFLIES |
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ICAS2020_0899: G.Y. Li, AVIC Xi'an Aircraft Industry Group Company LTD., China; T. Miao¹, B. Chen¹, F. Liu¹; ¹China Aerodynamics Research and Development Center, China AERODYNAMIC COEFFICIENT RESPONSE OF RECEIVER DURING AERIAL REFUELING PROCESS |
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ICAS2020_0285: J. Su, China; Z. Tang, China; J. Tian, China; B. Pan, China; S. Luo, China CFD OPTIMUM DESIGN OF SUPERSONIC EJECTOR SYSTEM STRUCTURE OF TEST CELL |
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ICAS2020_0845: H. Chen¹, Y.F. Yang¹, P. Xue¹, X.X. Li¹, C. Dong¹, S.Z. Wang¹, M.X. Zhang¹; ¹Beijing Institute of Space Long March Vehicle, China INVESTIGATION ON DIFFERENT NUMERICAL SIMULATION METHODS OF ROCKET ENGINE |
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ICAS2020_1125: S.-Z. Zhao¹, X. Zhao¹, K. You¹, M.-H. Kang¹, Y.-F. Lin, China Helicopter Research and Development Institute, China; ¹Northwestern Polytechnical University, China HELICOPTER ROTOR AERODYNAMIC PERFORMANCE PREDICTION BASED ON FLOW SIMULATION AROUND AIRFOILS |
3.2 - Experimental Aerodynamics |
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ICAS2020_0040: Q. Liu¹, Z. Luo¹, Z. Liu¹, X. Deng¹, P. Cheng¹; ¹National University of Defense Technology, China EXPERIMENTAL INVESTIGATION ON SUPERSONIC BOUNDARY LAYER TRANSITION INDUCED BY SINGLE/MULTI- ROUGHNESS ELEMENTS |
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ICAS2020_0182: X.W. Xu¹, S.H. Yi¹, J.H. Han¹, W.P. Zheng¹, Z.H. Xia¹; ¹National University of Defense Technology, China EXPERIMENTAL INVESTIGATION OF HYPERSONIC BOUNDARY LAYER TRANSITION ON A SHARP CONE UNDER DIFFERENT ANGLES-OF-ATTACK |
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ICAS2020_0500: X. Li¹, Z. Liu¹, Z. Qian¹; ¹AVIC Aerodynamics Research Institute, China A STUDY OF SONIC BOOM TEST WITH NOZZLE PLUME INTERACTIONS |
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ICAS2020_0140: Z.-B. Zhang¹, M.-S. Yang¹, H. Wu¹, M. Wang¹; ¹Shenyang Engine Research Institute, China EXPERIMENTAL INVESTIGATION ON FLOW CHARACTERISTICS IN COMPRESSOR ACOUSTIC-CAVITY RESONANCE TEST FACILITY BY PIV |
3.3 - Basic Fluid Dynamics and Flow Control |
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ICAS2020_1189: J.J. Yang¹, Y.D. Zhang¹, P. Lv¹, T. Pagliaroli, Università Niccolò Cusano, Italy; ¹China Academy of Aerospace Aerodynamics, China NUMERICAL SIMULATION OF LOCAL LONG SHALLOW CAVITY EFFECT ON THE STABILITY OF A HYPERSONIC BOUNDARY LAYER |
3.4 - Applied Aerodynamics |
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ICAS2020_1183: J.X. Gao¹, W.Q. Yang¹, R. Zhang¹, Y.B. Li¹; ¹Northwestern Polytechnical University, China NUMERICAL SIMULATION ON AERODYNAMIC PERFORMANCE OF BIRD-LIKE FLAPPING WING LEADING EDGE COVERTS |
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ICAS2020_1240: R. Zhang¹, W.Q. Yang¹, Y.B. Li¹, J.X. Gao¹; ¹School of Aeronautics, Northwestern Polytechnical University, China NUMERICAL SIMULATION OF VARIABLE WINGSPAN EFFECTS ON A BIONIC FLAPPING WING |
4.1 - Material Issues, Fatigue and Damage Tolerance |
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ICAS2020_0833: D. Wei¹, Y. Cui¹, Y.A. Shi¹, G.M. Xiao¹, Y.X. Du¹, Y.W. Gui¹; ¹China Aerodynamics Research and Development Center, China A NEW METHOD FOR ESTIMATING THE THERMOS-PHYSICAL PARAMETERS OF THERMAL PROTECTION MATERIALS BY ULTRASONIC MEASUREMENTS |
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ICAS2020_0118: S. Su¹, W. Zhang¹, L. Li¹; ¹Aircraft Strength Research Institute, China FRACTURE CRITERION ANALYSIS AND CRACK GROWTH PROPERTY OF MIXED-MODE CRACK EXPERIMENTS |
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ICAS2020_0904: Y.J. Wang¹, Y. Liao¹, H. Dui¹, J. Dong¹; ¹Chengdu Aircraft Design and Research Institute, China STUDY ON THE FATIGUE SCATTER FACTOR UNDER SEVERE LOAD SPECTRUM |
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ICAS2020_1203: L.F. Wang¹, L. Liu², C. Liu, Jiangsu Aero-XY Technology Co., Ltd, China; X.L. Pan¹, Z.H. Zhao², L.C. Zhou¹; ¹Air Force Engineering University, China; ²Nanjing University of Aeronautics and Astronautics, China RESEARCH ON FATIGUE STRENGTH PREDICTION MODEL OF AERO-ENGINE BLADES SUBJECTED TO FOREIGN OBJECT DAMAGE |
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ICAS2020_1065: D. Jin¹, G.P. Qian¹, K. Feng¹; ¹Shanghai Aircraft Design and Research Institute, China STUDY ON THE METHOD OF DETERMINING SKIN WAVINESS REQUIREMENT OF CIVIL AIRCRAFT |
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ICAS2020_0713: Y.L. Su¹, Z.L. Fan¹, W.H. Wu¹, S. Lu, Northwestern Polytechnical University, China; X.M. Chen, Aircraft Strength Research Institute of AVIC, China; ¹China Aerodynamics Research and Development Center, China DESIGN METHOD FOR THE FATIGUE-SIMULATING SPECIMEN OF TWIN-WEB TURBINE DISK |
4.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity |
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ICAS2020_0880: S.Q. Bi¹, H. Cui¹, L.Y. Liu¹; ¹Shenyang Aircraft Design and Research Institute of AVIC, China THE FINITE ELEMENT MODELLING OF BOLTED STRUCTURE BETWEEN SELECTIVE LASER MELTING ALUMINIUM AND COMPOSITE PLATES |
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ICAS2020_0599: F. Chen¹, P. Chen¹, Y.Q. Zhao¹; ¹Shanghai Aircraft Manufacturing Corporation Ltd, China DEFORMATION ANALYSIS OF C-SPAR COMPOSITE STRUCTURE DURING THE PREFORMING PROCESSING |
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ICAS2020_0731: Y. Ding, China; Z. Zhou, China; H.J. Liu, China BIONIC LIGHT-WEIGHT GRID SURFACE WING STRUCTURE DESIGN FOR A SOLAR-POWERED UAV |
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ICAS2020_0208: X.Y. Pang, China; W.W. Men, China; J.F. Huang, China DESIGN AND PERFORMANCE RESEARCH OF ARTIFICIAL ELECTROMAGNETIC STRUCTURE WITH TRANSMISSION AND ABSORPTION CHARACTERISTICS |
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ICAS2020_0924: L. Magerramova, Central Institute of Aviation Motors, Russia; E. Kratt, Laboratory of New Technology, Russia DEVELOPMENT OF ADVANCED DESIGNS OF GAS TURBINE ENGINES FROM POWDER COMPOSITIONS |
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ICAS2020_0360: D. Gueraiche¹, S. Popov¹, A. Guelailia, Space mechanical research development, Algeria; ¹Moscow Aviation Institute, Russia PASSIVE FLEXIBLE WINGTIP AREA FOR IMPROVING AIRLINERS CRUISE EFFICIENCY AND GUST ALLEVIATION |
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ICAS2020_0187: C. Chang¹, J. Li¹; ¹China helicopter research and development institute, China DESIGN AND VERIFICATION OF ENERGY-ABSORBING STRUCTURE OF CORRUGATED BEAM BASED ON SPECIFIC FAILURE MODE |
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ICAS2020_0393: K. Yuan¹, M. Cheng¹; ¹Beijing Electro-Mechanical Engineering Institute, China SUPERSONIC AEROELASTIC ANALYSIS OF AN ALL-MOVABLE WING WITH FREE PLAY |
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ICAS2020_0780: H.-C. Qiu¹, W.-C. Fan¹, Y.-N. Fang¹; ¹COMAC Shanghai Aircraft Manufacturing Co., Ltd., China IMPROVED STOCHASTIC PERTURBATION ALGORITHM FOR GENERALIZED REPEATED EIGENVALUES PROBLEM BASED ON SURROGATE MODEL |
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ICAS2020_0392: Y. Liu¹, D. Zhou¹, S. Feng¹, C. Yang¹, H. Xie¹; ¹Chengdu Aircraft Industry (Group) Corporation Ltd., China PROCESS RESEARCH AND OPTIMINZATION OF PINHOLE HOLE AND NAIL HEAD DAMAGE ON COMPOSITE PARTS |
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ICAS2020_0086: P. LI, Aircraft Strength Research Institute, China TRANSFER PATH ANALYSIS OF RANDOM VIBRATION LOADS |
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ICAS2020_0308: Z. Jia, China; L. Xuan, China; T. Su., China; L. Chen, China BROADBAND MICROWAVE ABSORBING HONEYCOMB CORE MATERIAL WITH ACTIVE CARBON AS DELEGATES |
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ICAS2020_0391: W.-J. Nie¹, W.-Q. Deng¹, Y.-N. Chen¹, L. Zou¹; ¹AECC Hunan Aviation Powerplant Research Institute , China TURBINE STRUCTURE ANALYSIS AND IMPROVEMENT OF A HIGH-SPEED ROTOR WITH MULTI-DISK AND MULTI-SUPPORT |
5 - Propulsion |
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ICAS2020_1122: C.-H. Liang¹, M.-B. Sun¹, Y.-X. Yang¹, Y. Liu, China Aerodynamics Research and Development Center, China; T.-Y. Wang¹, G.-W. Ma¹, F. Li¹, C. Wang¹; ¹National University of Defense Technology, China EXPERIMENTAL STUDY ON THE CHARACTERISTICS OF SONIC GAS INJECTION INTO SUPERSONIC CROSSFLOW WITH MA2.0 AND MA3.0 |
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ICAS2020_0722: J. Jiao¹, X.-P. Ma¹, B.-F. Song, Northwestern Polytechnical University, China; J.-B. Yang, China Electronics Technology Group Corporation 38th Research Ins, China; ¹Chinese Academy of Sciences, China AERODYNAMIC AND STRUCTURAL DESIGN OF THE COMPOSITE PROPELLER FOR NEAR SPACE VEHICLES |
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ICAS2020_0290: H. Li, Aero Engine Corporation of China, China; C. Liang¹, X. Li¹; ¹AECC Shenyang Engine Research Institute, China MODELING AND SIMULATION APPLICATION THROUGHOUT THE AERO-ENGINE LIFE CYCLE |
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ICAS2020_1146: X. Yang¹, Z.-W. Wang¹, Y.-B. Niu¹, H.-Y. Miao¹; ¹college of aerospace science and engineering,national university, China INFLUENCE OF SHOCK TRAIN ON HEAT FLUX DISTRIBUTION OF A CIRCULAR CONSTANT-AREA ISOLATOR |
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ICAS2020_0257: Y.F. Li¹, Z.Z. Na¹, Y. Chen¹, Y.B. Wang¹; ¹AECC, China EFFECT OF COMPLEX FLOW PROFILES AT COMBUSTOR EXIT ON TURBINE CHARACTERISTICS |
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ICAS2020_1100: Y.-H. Wang¹, G.-P. Qian¹; ¹Shanghai Aircraft Design and Research Institute, China NUMERICAL STUDY OF HIGH TEMPERATURE TRANSVERSE PULSE JET IN THE SUPERSONIC COMBUSTION CHAMBER |
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ICAS2020_0504: M. Zhang, AECC Commercial Aircraft Engine, China NUMERICAL INVESTIGATION OF NACELLE INTAKE FLOW DISTORTION AT CROSSWIND CONDITIONS |
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ICAS2020_0160: X. Yang¹, Q. Yang¹, W. Dong¹; ¹Shanghai Jiao Tong University, China A SIMPLIFIED MODEL FOR THE SIMULATION OF SYNERGISTIC AIR-BREATHING ROCKET ENGINE |
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ICAS2020_0544: C. Hu¹, J. Gu¹, F. Gao¹; ¹AVIC The First Aircraft Institute, China THE RESEARCH ON PROPELLER NOISE PREDICTION METHOD FOR TURBOPROP AIRCRAFT |
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ICAS2020_1099: S.C. Xu¹, Y. Wang¹, Z.G. Wang¹, X.Q. Fan¹, B. Xiong¹; ¹National University of Defense Technology, China A DESIGN METHOD OF AN AXISYMMETRIC HYPERSONIC INLET INTERGRATED WITH A LONG FOREBODY |
6.1 - Flight Dynamics and Control (Control & Modelling) |
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ICAS2020_0073: T. Rogalski¹, P. Rzucidlo¹, J. Prusik, Doctoral School of Engineering and Technical Sciences at Rzeszo, Poland; ¹Rzeszow University of Technology, , Poland AIRCRAFT FLIGHT CONTROL SYSTEM FOR AEROBATIC FLIGHT |
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ICAS2020_0418: D.-N. Liu¹, W.-K. Wang¹, B.-D. Zhao¹, X.-Z. Hu¹, B.-W. Nie¹; ¹China Aerodynamics Research and Development Center, China PRELIMINARY VIRTUAL FLIGHT VALIDATION OF A QUAD TILT ROTOR UAV IN WIND TUNNEL |
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ICAS2020_0865: H.Y. Shi¹, H. Xie², X. Hu¹, Y.M. Liu¹, Z.Y. Cai², H.J. Zhao², Y.M. Zhou¹; ¹Beihang University, China; ²AVIC General Huanan Aircraft Industry Co., Ltd., China RESEARCH AND DESIGN OF AMPHIBIOUS AIRCRAFT FIRE-EXTINGUISHING SIMULATION MANAGEMENT SYSTEM BASED ON DIS |
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ICAS2020_1001: O. Kreerenko, Moscow Aviation Institute, Beriev Aircraft Company, Russia SYNERGETIC CONTROLS OF THE SYSTEM “CARRIER AIRCRAFT - UPPER-STAGE ROCKET“ |
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ICAS2020_1104: Y. Kong¹, K. He¹, M.H. Lowenberg², S.A. Neild², F. Cen¹; ¹China Aerodynamics Research and Development Center, China; ²University of Bristol, United Kingdom NONLINEAR UNSTEADY AERODYNAMIC MODELING AND LONGITUDINAL STABILITY ANALYSIS FOR AN AIRCRAFT MODEL |
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ICAS2020_0525: Y. Liu¹, B.-G. Mi, Shanghai Aircraft Airworthiness Certification Center, China; X. Liu¹, H. Zhan¹; ¹Northwestern Polytechnical University, China MODELING AND DYNAMICS STABILITY ANALYSIS FOR A BLENDED-WING-BODY AIRCRAFT |
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ICAS2020_1266: Z.-Y. Wang¹, P. Chen¹, Y.-L. Wang¹, W.-D. Huang¹; ¹Aerospace Engineering University, China ASCENT TRAJECTORY OPTIMIZATION OF HYPERSONIC VEHICLE USING SWARM INTELLIGENT METHOD |
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ICAS2020_0448: S.V. Serokhvostov, MIPT, Russia; T.E. Churkina, MAI, Russia OPTIMAL TRAJECTORY DEPENDENCE ON THE ATMOSPHERE MODEL FOR THE SUN-POWERED AIRPLANE |
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ICAS2020_0978: L. Zheng¹, Z. Bai¹, Z. Zhou¹, R. Wang¹; ¹Northwastern Polytechnical University, China APPLICATION OF VECTOR JET CONTROL TECHNOLOGY ON AIRCRAFT LONGITUDINAL CONTROL |
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ICAS2020_0948: L.-F. Chang¹, G.-L. Xue¹, Z.-W. Liu¹; ¹China Aeronautical Radio Electronics Research Institute, China A METHOD OF MANEUVER IDENTIFICATION AND TRAJECTORY PREDICTION FOR AGILE TARGET |
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ICAS2020_0197: C. Qi, China Aeronautical Radio Electronics Research Institute, China L1 ADAPTIVE CONTROL AUGMENTATION FOR A FLEXIBLE AIR-BREATHING HYPERSONIC VEHICLE MODEL |
6.2 - Flight Dynamics and Control (UAV related) |
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ICAS2020_1228: D. Ning¹, Y. Wang¹, S. Jia¹; ¹China Academy of Aerospace Aerodynamics, Beijing, China, China A POLE CONFIGURATION CONTROLLER FOR FIXED HEIGHT CONTROL OF TILT ROTOR AIRCRAFT |
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ICAS2020_0282: G.F. Yu, School of Software, Northwestern Polytechnical University, China; L. Zhang¹, C.H. Zou¹, Y.C. Liu, Beijing Aerospace Automatic Control Institute, China; Y. Cheng¹; ¹AVIC Xi’an Aeronautics Computing Technique Research Institute, China A ROBUST AND REAL-TIME VISUAL-INERTIAL POSE ESTIMATION FOR FIX-WING AIRCRAFT LANDING |
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ICAS2020_1006: T.L. Costa¹, J.C. Vendrichoski¹, E.S. El'Youssef¹, E.R. De Pieri¹; ¹Federal University of Santa Catarina, Brazil ROBUST CONTROL OF UNMANNED AERIAL VEHICLE WITH TILT ROTORS AND CAMERA |
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ICAS2020_0651: M.H. Sadraey, Southern New Hampshire University, United States ROCKETS HYBRID LAUNCH SYSTEM USING LINEAR SYNCHRONOUS ELECTRIC MOTORS |
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ICAS2020_1088: W.Y. Zhou¹, S.M. He¹, M.M. Tian¹; ¹AVIC Xi’an Flight Automatic Control Research Institute, China ADRC BASED HIGH MANEUVERING FLIGHT CONTROL LAW DESIGN FOR UAV |
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ICAS2020_0619: R. Wang¹, J.-N. Du¹, Z. Xiong¹, J.-Y. Liu¹, Y. Rui¹, T.-Y. Nie¹; ¹Nanjing University of Aeronautics and Astronautics, China EXPERIMENTAL RESEARCH OF COOPERATIVE NAVIGATION METHOD FOR CLUSTER AIRCRAFTS BASED ON MUTUAL DISTANCE DIFFERENCE MODEL |
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ICAS2020_0769: A. Satoh, Iwate University, Japan; M. Watanabe, O.T.Techno Research Co., Ltd., Japan; K. Hozumi¹, A. Watanabe¹; ¹Japan Aerospace Technology Foundation (JAST), Japan ENDURANCE ANALYSIS OF BATTERY-POWERED MULTICOPTERS: DERIVATION OF PROPER CUT-OFF VOLTAGE USING DC MOTOR MODEL |
7 - Systems, Subsystems and Equipment |
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ICAS2020_1114: X.C. Li¹, H.F. Wei¹, J.M. Wu¹, F. Liu¹; ¹ADR (Aviation Industry Development Research Center of China), China A MANUFACTURING COST ESTIMATION MODEL WITH RELIABILITY FOR CIVIL AERO-ENGINE |
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ICAS2020_0292: C.-L. Han¹, F. Chen¹, X.-M. Sun¹, W.-H. Li¹; ¹China National Aeronautical Radio Electronics Research Institute, China FLIGHT MANAGEMENT SYSTEM REQUIREMENT ANALYSIS FOR TRAJECTORY BASED OPERATION |
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ICAS2020_0273: W.-J. Mo¹, X.-X. Huang¹, J.-A. Cao, School of Electrical Engineering, Xi’an Jiaotong University, China; Q. Yin¹, X.-H. Wu¹; ¹Chengdu Aircraft Industrial (Group) Co. Ltd, China RESEARCH ON AIRBORNE RF SYSTEM TESTING TECHNOLOGY USING TDR TECHNIQUE |
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ICAS2020_0822: K.T. Li¹, H.S. Ma¹, D. Wang¹; ¹China National Aeronautical Radio Electronics Research Institute, China DESIGN OF UAV NAVIGATION ALGORITHM IN SINGLE SATELLITE ENVIRONMENT BASED ON HIGH PRECISION TIMING |
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ICAS2020_0344: Z. Liu¹, P. Chen¹, X. Wei¹; ¹Xi'an Flight Automatic Control Research Institute, China MEMS-BASED DISTRIBUTED NAVIGATION SYSTEM |
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ICAS2020_0808: C. Chen¹, J.S. Shen¹, Q.C. Liu¹, B. Xue¹; ¹China Aeronautical Radio Electronics Research Institute, China PRECISION ANALYSIS AND INDEX DISTRIBUTION SYSTEM DESIGN OF AVIONICS SYSTEM BASED ON BP NEURAL NETWORK |
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ICAS2020_1018: B. Wu¹, X. Qui¹, Y. Zhu, COMAC SADRI, China; ¹NUAA, COMAC SADRI, China BASED ON SYSTEMS ENGINEERING PROCESS THE CIVIL AIRCRAFT PROJECT PRODUCT BREAKDOWN STRUCTURE DEVELOPMENT RESEARCH |
8 - Manufacturing and Supply Chain Management |
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ICAS2020_0542: X. Zhu¹, H. Wang¹, L. Liu¹; ¹Chengdu Aircraft Industrial (Group) Co., Ltd, China ASSEMBLY QUALITY OPTIMIZATION APPROACH FOR LARGE-SCALE ACTIVE COMPONENTS BASED ON REVERSE ENGINEERING |
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ICAS2020_1223: L.S. Luna¹, G.A.P. Caurin¹, M.L. Tronco¹; ¹University of São Paulo, Brazil USAGE OF MQTT, ROS, AND AWS IN THE MANUFACTURING PROCESS OF AIRCRAFTS |
9 - Air Transport System Efficiency |
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ICAS2020_0207: V. Papantoni¹, J. Scherer¹, P. Wassink¹, G. Atanasov¹; ¹German Aerospace Center (DLR), Germany ASSESSMENT OF THREE COMMUTER AIRCRAFT CONCEPTS FROM A TRANSPORT SYSTEM PERSPECTIVE |
10 - Safety and Security |
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ICAS2020_1061: K. Tong¹, Y. Song¹, X.-F. Kong¹, K.-W. Zhang¹, Z.-J. Chen¹; ¹Civil Aviation University of China, China AN INTEGRATED METHOD FOR ACCURATE IDENTIFICATION AND DYNAMIC MONITORING OF BUILDINGS IN AERODROME OBSTACLE FREE SPACE |
11 - Operations and Sustainment |
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ICAS2020_0052: R.P. Liu, China; Q. Wang, China; G.Y. He, China; M.T. Tang, China; J.X. Ren, China THE DATABASE DESIGN OF UNMANNED AERIAL VEHICLE |