7th Asia-Pacific International Symposium on Aerospace Technology (APISAT 2015)

Similar documents
HYDROGEN FAST FILLING TO A TYPE IV TANK DEVELOPED FOR MOTORCYCLES

JOURNAL PUBLICATIONS

The Aerodynamic Design and Investigation of Loading Distribution of a Mixed Flow Compressor

Complex Systems and Applications

Fabrication of Novel Lamellar Alternating Nitrogen-Doped

High performance carbon nanotube based fiber-shaped. supercapacitors using redox additives of polypyrrole and. hydroquinone

SIMULATION OF ENVIRONMENTAL FLIGHT CONDITIONS

Development of Technology to Estimate the Flow Field around Ship Hull Considering Wave Making and Propeller Rotating Effects

Tim Lee s journal publications

Experimental research on instability fault of high-speed aerostatic bearing-rotor system

Research on Small Wind Power System Based on H-type Vertical Wind Turbine Rong-Qiang GUAN a, Jing YU b

The Study on the Influence of Gust Wind on Vehicle Stability Chen Wang a, Haibo Huang b*, Shaofang Xu c

Interconnected hierarchical NiCo 2 O 4 microspheres as high performance. electrode material for supercapacitor

STUDY OF MODEL DEFORMATION AND STING INTERFERENCE TO THE AERODYNAMIC ESTIMATIONS OF THE CAE-AVM MODEL

Layered polyaniline/graphene film from sandwich-structured polyaniline/graphene/polyaniline nanosheets for high-performance pseudosupercapacitors

Analysis of wind resistance of high-rise building structures based on computational fluid dynamics simulation technology

Aggregation modeling of large wind farms using an improved K-means. algorithm

Numerical simulation of aerodynamic performance for two dimensional wind turbine airfoils

Modal Analysis of Propulsion Shafting of a 48,000 tons Bulk Carrier

Numerical Investigation of Air Bubbles Evolution and Coalescence from Submerged Orifices Based on OpenFOAM

Investigation on Divergent Exit Curvature Effect on Nozzle Pressure Ratio of Supersonic Convergent Divergent Nozzle

RECENT ADVANCES IN WIND ENGINEERING

Hierachical Nickel-Carbon Structure Templated by Metal-Organic Frameworks for Efficient Overall Water Splitting

2012 International Conference on Future Energy, Environment, and Materials

Numerical simulation and analysis of aerodynamic drag on a subsonic train in evacuated tube transportation

The Usage of Propeller Tunnels For Higher Efficiency and Lower Vibration. M. Burak Şamşul

NUMERICAL SIMULATION OF STATIC INTERFERENCE EFFECTS FOR SINGLE BUILDINGS GROUP

Lecture # 08: Boundary Layer Flows and Drag

Effect of attack angle on flow characteristic of centrifugal fan

Supporting Information

A Distributed Control System using CAN bus for an AUV

Numerical Simulation And Aerodynamic Performance Comparison Between Seagull Aerofoil and NACA 4412 Aerofoil under Low-Reynolds 1

Keywords: contra-rotating fan, air pressure, deformation of blades.

Finite Element Modal Analysis of Twin Ball Screw Driving Linear Guide Feed Unit Table

Aerodynamic Shape Design of the Bow Network Monitoring Equipment of High-speed Train

state asymmetric supercapacitors

Aerodynamic Performance of 160km Box Car

A COMPUTATIONAL STUDY ON THE DESIGN OF AIRFOILS FOR A FIXED WING MAV AND THE AERODYNAMIC CHARACTERISTIC OF THE VEHICLE

Supporting Information. In-Situ Facile Bubble-Templated Fabrication of New-Type Urchin-Like (Li, Mo)- Doped Lix(Mo0.3V0.7)2O5 for Zn 2+ Storage

Vibration Analysis and Test of Backup Roll in Temper Mill

Aerodynamic Performance Comparison of Head Shapes for High-Speed Train at 500KPH

The effect of back spin on a table tennis ball moving in a viscous fluid.

Numerical and Experimental Investigations of Lift and Drag Performances of NACA 0015 Wind Turbine Airfoil

AE Dept., KFUPM. Dr. Abdullah M. Al-Garni. Fuel Economy. Emissions Maximum Speed Acceleration Directional Stability Stability.

Basketball field goal percentage prediction model research and application based on BP neural network

Supporting Information

MXene/Graphene Hybrid Fibers for High. Performance Flexible Supercapacitors

AERODYNAMIC CHARACTERISTICS OF NACA 0012 AIRFOIL SECTION AT DIFFERENT ANGLES OF ATTACK

WESEP 594 Research Seminar

ME 239: Rocket Propulsion. Forces Acting on a Vehicle in an Atmosphere (Follows Section 4.2) J. M. Meyers, PhD

Anna University Regional office Tirunelveli

CHAPTER 1 INTRODUCTION

CYCLE ANALYSIS OF LINEAR COMPRESSORS USING THREE- DIMENSIONAL CFD

Supporting Information. Mitigating the P2 O2 phase transition of high-voltage

Supporting Information

Stress Analysis of The West -East gas pipeline with Defects Under Thermal Load

Applied Fluid Mechanics

Supplementary Information. High areal capacity lithium sulfur battery cathode by. site-selective vapor infiltration of hierarchical

Howard Torode. Member of General Aviation Group and Chairman BGA Technical Committee

Flight Corridor. The speed-altitude band where flight sustained by aerodynamic forces is technically possible is called the flight corridor.

1. Numerical simulation of AGARD WING 445.6

OPTIMIZATION OF INERT GAS FLOW INSIDE LASER POWDER BED FUSION CHAMBER WITH COMPUTATIONAL FLUID DYNAMICS. Abstract. Introduction

CFD AND EXPERIMENTAL STUDY OF AERODYNAMIC DEGRADATION OF ICED AIRFOILS

Supporting Information. Metal organic framework-derived Fe/C Nanocubes toward efficient microwave absorption

Vibration measurement method of the ship propulsion shafting

Design & Analysis of Natural Laminar Flow Supercritical Aerofoil for Increasing L/D Ratio Using Gurney Flap

Wind tunnel effects on wingtip vortices

Unsteady Aerodynamics of Tandem Airfoils Pitching in Phase

AIRFLOW GENERATION IN A TUNNEL USING A SACCARDO VENTILATION SYSTEM AGAINST THE BUOYANCY EFFECT PRODUCED BY A FIRE

THEORETICAL EVALUATION OF FLOW THROUGH CENTRIFUGAL COMPRESSOR STAGE

Impact of Turbulence on Unmanned Aerial Vehicles

Analysis of the Impact of Rotor Rigidity on the Aerodynamic Performance of Vertical Axis Wind Turbines

THE PERFORMANCE OF PLANING HULLS IN TRANSITION SPEEDS

Conventional Ship Testing

5th Symposium on Integrating CFD and Experiments in Aerodynamics (Integration 2012) th Symposium on Integrating CFD and Experiments in Aerodynam

Experimental study on aerodynamic characteristics of vertical-axis wind turbine

Octahedral Pd Nanocages with Porous Shells Converted by Co(OH) 2 Nanocages with Nanosheet surface as Robust Electrocatalysts for Ethanol Oxidation

Electronic Supplementary Information (ESI)

A Research on the Airflow Efficiency Analysis according to the Variation of the Geometry Tolerance of the Sirocco Fan Cut-off for Air Purifier

Study on Water Hammer Prevention in Pumping Water Supply Systems by Multi-valves

A reformative oxidation strategy using high concentration nitric acid for. enhancing emission performance of graphene quantum dots

Supporting Information for

683. Design and analysis of a ducted fan UAV

A Correlation Study of Nadal's and Federer's Technical Indicators in Different Tennis Arenas

On the use of rotor equivalent wind speed to improve CFD wind resource mapping. Yavor V. Hristov, PhD Plant Performance and Modeling Vestas TSS

Surrounding buildings and wind pressure distribution on a high rise building

In parallel with steady gains in battery energy and power density, the coming generation of uninhabited aerial vehicles (UAVs) will enjoy increased

The Application of Pedestrian Microscopic Simulation Technology in Researching the Influenced Realm around Urban Rail Transit Station

ITTC Recommended Procedures Testing and Extrapolation Methods Manoeuvrability Free-Sailing Model Test Procedure

EXPERIMENTAL ANALYSIS OF FLOW OVER SYMMETRICAL AEROFOIL Mayank Pawar 1, Zankhan Sonara 2 1,2

Aerodynamic Analysis of Small Propeller in Wind Field Using CFD Chuansheng Zhang1, a, Shengguang Xie2,b and Tianhao Qin3,c

Effects of Air Injection on Aerodynamic Performance of a Single-Stage Transonic Axial Compressor

A. M. Dalavi, Mahesh Jadhav, Yasin Shaikh, Avinash Patil (Department of Mechanical Engineering, Symbiosis Institute of Technology, India)

Measurement and simulation of the flow field around a triangular lattice meteorological mast

Lecture # 08: Boundary Layer Flows and Controls

NUMERICAL INVESTIGATION OF THE FLOW BEHAVIOUR IN A MODERN TRAFFIC TUNNEL IN CASE OF FIRE INCIDENT

Supplementary Information. O-vacancy Enriched NiO Hexagonal Platelets Fabricated on Ni. Foam as Self-supported Electrode for Extraordinary

Performance Improvements in Boeing/AFOSR Mach 6 Quiet Wind Tunnel Based on CFD Predictions

«DO160/ED14» - Jessica France

FAI Sporting Code. UAV Class U. Section 12 Unmanned Aerial Vehicles Edition. Effective 1st January 2019

Transcription:

7th Asia-Pacific International Symposium on Aerospace Technology (APISAT 2015) Cairns, Australia 25 27 November 2015 ISBN: 978-1-5108-2431-7

Printed from e-media with permission by: Curran Associates, Inc. 57 Morehouse Lane Red Hook, NY 12571 Some format issues inherent in the e-media version may also appear in this print version. Copyright (2015) by Engineers Australia All rights reserved. Printed by Curran Associates, Inc. (2016) For permission requests, please contact Engineers Australia at the address below. Engineers Australia Engineering House 11 National Circuit Barton ACT 2600 Australia Phone: +61 2 6270 6555 Fax: (02) 6273 1488 www.engineersaustralia.org.au Additional copies of this publication are available from: Curran Associates, Inc. 57 Morehouse Lane Red Hook, NY 12571 USA Phone: 845-758-0400 Fax: 845-758-2633 Email: curran@proceedings.com Web: www.proceedings.com

TABLE OF CONTENTS THE SIMULATION OF REFUELING DROGUE MOVEMENT AT DIFFERENT REFUELING DOCKING VELOCITIES... 1 L. Chen, X. Liu EXPERIMENTAL STUDY ON MECHANICAL CHARACTERISTICS OF ORNITHOPTER WING... 10 H. Endo, H. Fujii RESEARCH ON COHERENCE OF UNSTEADY FLOW OF MULTI-ELEMENT AIRFOIL... 16 Y. Jiao, N. Xiong NUMERICAL SIMULATION OF ROUGHNESS-INDUCED BOUNDARY LAYER TRANSITION... 23 H. Li, Y. Zheng WHIRL FLUTTER AND ROTOR HUB CENTER'S MOTION IMAGE OF TILTROTOR AIRCRAFT... 30 Z. Li, P. Xia PROGRESSIVE FAILURE ANALYSIS FOR LOW-VELOCITY IMPACT OF COMPOSITE SANDWICH PLATES BASED ON LAYERWISE/SOLID-ELEMENTS (LW/SE) METHOD... 42 D. Li, Y. Liu, X. Zhang DESIGN FOR FAULT TOLERANT PERMANENT MAGNET MOTOR CONTROL SYSTEM... 59 Z. Hao, S. Yu SERIES HYBRID-ELECTRIC PROPULSION FOR FIXED-WING VTOL UAV... 66 J. Bak, S. Cho, K. Park, S. Won, G. Lee, L. Cho, C. Moon, J. Cho A FINITE VOLUME METHOD FOR FULL-POTENTIAL EQUATION ON ADAPTIVE CARTERSIAN GRIDS... 80 F. Lv, X. Yu, T. Xiao CALCULATION STUDY OF HEAT GENERATION IN COUNTER-ROTATING CYLINDRICAL ROLLER BEARING... 91 P. Zhu, Z. Liu, W. Gao, J. Zhao, Y. Lu AEROSPACE DESIGN - A NEW WORLD THANKS TO DIGITAL TECHNOLOGY... 98 J. Page, J. Olsen COMPUTATION AND ANALYSIS OF LATERAL-DIRECTIONAL DYNAMIC DERIVATIVES OF THE NEAR SPACE SOLAR POWERED AIRCRAFT... 104 C. Ye, F. Li, G. Li DEVELOPMENT OF HARDWARE-IN-THE-LOOP SIMULATOR FOR EXPERIMENTAL WINGED ROCKET... 114 K. Shirakata, K. Yonemoto, H. Yamasaki, Y. Ura, H. Minote, A. Shiihara, S. Ohmori, S. Ishimoto, T. Mugitani THE STABILITY STUDY OF THE CONSTANT TEMPERATURE HOT-WIRE ANEMOMETER CONTROL CIRCUIT... 121 T. Zhang, H. Chen, Q. Wei, H. Jin THE PERFORMANCE STUDY OF AXIAL BREATHER WITH HONEYCOMB IN THE AERO- ENGINE LUBRICATION SYSTEMS... 128 J. Zhao, Z. Liu, P. Zhu, Y. Lu, G. Ren THE RESEARCH ON THE REAL-TIME AND FULL-ENVELOPED MODEL IDENTIFICATION OF TURBOFAN ENGINE S HYDRO-MECHANICAL ACTUATOR... 133 H. Xiao, W. Li, H. Li A FLUTTER BOUNDARY PREDICTION TECHNIQUE UNDER ATMOSPHERIC TURBULENCE EXCITATION... 137 Y. Li, L. Zhou, B. Yang NUMERICAL SIMULATION OF REBOUND CHARACTERISTICS OF SAND PARTICLES IMPACTING ON METAL PLATE... 148 J. Fan, T. Wu THE RESEARCH OF AEROSTAT GROUND TEST BASED ON ROCKET SLED TECHNIQUES... 157 S. Huang, J. Liu, S. Huang, J. Liu RESEARCH ON ATMOSPHERIC ENTRY PILL FOR THE UPPER ATMOSPHERE OBSERVATION... 168 K. Sakuyama, H. Sahara, M. Watanabe INVESTIGATION ON INFLUENCE OF BRAID ANGLE AND BOUNDARY CONDITION FOR IMPACT RESPONSE OF TRIAXIAL BRAIDED COMPOSITES WITH SUBCELL MODEL USING SOLID ELEMENTS... 174 H. Tan, L. Liu, Y. Guan, W. Chen, Z. Zhao

MATCHING CALCULATION AND PERFORMANCE ANALYSIS FOR AERO-ENGINE STARTING AIR FEEDING SYSTEM... 183 X. Huang, X. Zhao EFFECT OF ROTATIONAL DIRECTION OF TRIPLE-SWIRLER ON COLD FLOW CHARACTERISTICS... 192 X. He, Z. Zhao DEVELOPMENT OF A DYNAMIC PROPULSION MODEL FOR ELECTRIC UAVS... 206 A. Gong, D. Verstraete AIR COMBAT TACTICAL DECISION UNIT BASED ON FINITE STATE MACHINE... 218 H. Song, L. Xia, C. Shang, H. Zhan A METHOD OF MONOCULAR VISION BASED ASYNCHRONOUS ELEVATION MEASUREMENT FOR MUAV... 231 P. Wen, Y. Cheng, Y. Zhang, Y. Li AERODYNAMIC CHARACTERISTICS OF A DEPLOYABLE-WING AIRPLANE WITH AN ELEVON FOR MARS EXPLORATION... 241 G. Yamada, A. Miyazaki, H. Kawazoe AERODYNAMIC PARAMETERS ESTIMATION FOR REENTRY CAPSULE... 249 G. Wang, Z. Liu, Z. Liu, Y. Zhou RESEARCH AND VALIDATION OF GLOBAL SKIN FRICTION MEASUREMENT TECHNIQUES BASED ON FLUORESCENT OIL FILM... 258 Z. Huang, H. Wang, L. Wei ANALYSIS OF LOW SPEED STABILITY DERIVATIVES OF A HYPERSONIC TEST VEHICLE... 266 J. Leyaratnam, D. Verstraete PARAMETER OPTIMIZATION OF MULTISTAGE MISSILE FOR TERMINAL VELOCITY MAXIMIZATION... 276 J. Lee, S. Hong, Y. Kim, M. Tahk RESPONSE TIME ANALYSIS OF TTCAN BUS FOR AERO-ENGINE DISTRIBUTED CONTROL SYSTEM... 283 X. Fan, M. Pan, J. Huang NETWORK-BASED GUARANTEED COST TRACKING CONTROL FOR AERO-ENGINE... 292 R. Zhang, M. Pan, J. Huang ASSESSMENT OF NUMERICAL SIMULATION FOR UNDEREXPANDED SONIC JET ISSUED FROM AXISYMMETRIC CONVERGENT NOZZLES... 302 Y. Akita, S. Nakao, D. Ono, Y. Miyanto A STUDY ON AERODYNAMIC CHARACTERISTICS OF AIRCRAFT MODEL WITH VORTEX GENERATORS BY WAKE MEASUREMENTS... 309 M. Kashitani, Y. Yamaguhi, K. Kusunose, Y. Takita THE CHANGING SIZE OF THE COMMERCIAL AVIATION PASSENGER AND ITS POTENTIAL IMPACT ON THE AVIATION INDUSTRY... 319 D. Melis, J. Silva, R. Clothier EXPERIMENTAL ANALYSIS OF THE DYNAMIC CHARACTERISTICS OF AN ORNITHOPTER... 329 M. Kamii, H. Okubo, H. Fujii, H. Endo TESTS OF ALTERNATIVE FUEL BLENDS IN MICRO-TURBOJET ENGINES... 337 J. Vivian, A. Seeber, G. Dorrington RESEARCH ON THE TECHNOLOGY OF TURBOFAN ENGINE STARTING FAULT DIAGNOSIS... 343 Z. Tang, W. Zhou, J. Huang, Q. Zhang STUDY ON A MORPHING WING STRUCTURE USING OPEN-SECTION MEMBER... 352 A. Aso, H. Tanaka RESEARCH ON FIXED WING UAV FORCED LANDING TECHNOLOGY... 361 G. Yang, K. Song, X. Zhu, W. Wei RESEARCH TO IDENTIFY MATHEMATICAL MODELS OF QUADROTOR... 369 N. Dung, T. Hung AERODYNAMIC ANALYSIS OF AIRBORNE MAGNETIC GRADIENT MEASUREMENT APPLIED ON HIGH ASPECT RATIO-UAV... 378 Y. Fu, C. Jun, S. Tian CALCULATING DYNAMICS OF THE DAMPER SYSTEM FOR RECOVERING THE PAYLOAD IN A MODEL CARRIER ROCKET... 387 N. Dung, T. Hung

FLOW VISUALIZATION OF SEPARATION ON A SHROUDED ROTOR INLET IN A CROSSWIND... 395 H. Otsuka, K. Nagatani RECENT DEVELOPMENTS OF EXPERIMENTAL WINGED ROCKET: AUTONOMOUS GUIDANCE AND CONTROL DEMONSTRATION BY FLIGHT TEST... 408 T. Ohki, K. Yonemoto, M. Yamamoto, H. Yamazaki, M. Ichige, G. Surendra, S. Ishimoto, T. Mugitani AERODYNAMIC SHAPE OPTIMIZATION OF A BLENDED WING BODY AIRCRAFT WITH DISTRIBUTED PROPULSION SYSTEM... 415 W. Yan, J. Wu AN EXPLORATION OF SURFACE INTEGRITY REMANUFACTURING FOR AEROENGINE COMPONENTS... 422 X. Qian, H. Yong, T. Hou NAUTICAL TECHNOLOGY FOR AIRCRAFT EMERGENCY LOCATION TRACKING IN A MARITIME ENVIRONMENT... 431 L. Peters, C. Bil, P. Marazocca HYDRODYNAMIC RAM BEHAVIOUR IN RAM SIMULATOR... 444 H. Bae, K. Woo, I. Kim, J. Kim INTEGRATING PAIRWISE PROXIMITY-BASED AIR TRAFFIC CONTROL DIFFICULTY INDICES INTO AN AIRSPACE INDEX... 452 N/A THE VERIFICATION AND EXPERIMENT RESEARCH ON OPTICAL FLOW... 460 H. Wang, L. Wei, Z. Huang INTERMITTENT FAILURE DETECTION OF AVIATION ELECTRICAL CONNECTORS... 470 Z. Cai, S. Zhang EXPERIMENTS ON BUOYANCY AND CONDENSATION HEAT TRANSFER OF HELIUM OR AIR AND STEAM MIXTURES SUPPORTING VENUS AEROSTAT STUDY... 480 A. Herbert THE NOISE CREATED BY AN AIRFOIL IN THE WAKE OF A SUBBOUNDARY LAYER STEP... 490 D. Moreau, C. Doolan FLOW ANALYSIS OF THE EFFECT OF TUBE GEOMETRY ON THE PERFORMANCE OF PRE-COOLERS FOR TURBINE-BASED HYPERSONIC AIR-BREATHING PROPULSION... 500 T. Jones, N. Karwa, H. Ogawa, G. Rosengarten ERROR ANALYSIS WITH THE TRADITIONAL NUMERICAL METHOD OF THE LATERAL JET INTERACTION FOR THE SUPERSONIC FLOW... 510 L. Yang, Z. Ye LOAD INSTRUCTION STRATEGY OF DYNAMOMETER FOR STARTING PROCESS OF GAS TURBINE STARTERS... 523 X. Zhao, X. Huang INVESTIGATION OF STOCHASTIC SIMULATION INTO HELICOPTER STRUCTURAL CRASH AFTER AUTOROTATION SCENARIOS... 529 Y. Pei, J. Page, G. Pearce AIR TRAFFIC OPEN DATA AND ITS IMPROVEMENT... 537 Y. Fukuda, M. Oka, N. Wickramasinghe, K. Uejima A NUMERICAL RESEARCH ON AERODYNAMIC INTERFERENCE OF DIAMOND-WING SENSOR-CRAFT... 545 Z. Wang, X. Zhu, Z. Zhou, C. Zhang, Y. Wang LIMIT TESTING OF A FOAMED CONCRETE ARRESTOR'S RESISTANCE TO JET BLAST... 553 X. Xiao, Y. Shi, H. Yao VIBRO-ACOUSTIC COUPLING RESPONSE ANALYSIS AND NOISE CONTROL OF THE WINDOW AND CABIN OF AIRCRAFT BY APPLYING ACOUSTIC WAVEGUIDE MODAL EXPANSION METHOD... 558 S. Ning, Z. Shi, J. Zhang, D. Qian, J. Li SIMULATION RESULTS OF COOPERATIVE FORMATION FLYING CONTROL OF UAVS WITH COLLISION AVOIDANCE BASED ON ORCA... 569 A. Mello, R. Chiaramonte, L. Filho, R. Inoue, K. Branco CONVERGENCE TECHNOLOGY R&D FOR AIRCRAFT DESIGN WITH RESPECT TO AVIATION SAFETY AND GREEN AVIATION/AIRCRAFT... 577 S. Nah ACCURACY OF ONE-DIMENSIONAL HEAT TRANSFER MODEL OF RADIOISOTOPE THERMOELECTRIC GENERATOR... 584 J. Kim, J. Park, J. Hong, G. Son

A CASE STUDY FOR IMPROVING AIRCRAFT DEVELOPMENT PROJECTS: HOW DO STUDENTS MANAGE A TEAM UNDER THE CURRICULUM?... 593 J. Kumura, S. Suzuki DUAL FIELD ANALYSIS OF POLING DESIGN OF PVDF FIBRES FOR ENERGY HARVESTING APPLICATIONS... 604 S. Waqar, S. John, I. Khan, C. Wang, A. Ladigus-Grange, L. Wang, F. Coman A COMPUTATIONAL STUDY ON TAIL BUFFETING SUPPRESSION BY AN INFLATABLE BUMP... 613 Q. Zhang, Z. Ye UAV RECHARGING USING NON-CONTACT WIRELESS POWER TRANSFER... 624 M. Simic, C. Bil, V. Vojisavljevic, J. Perilla AN INTEGRATED DESIGN OF LIGHT-WEIGHT GRADED STRUCTURE FOR HYPERSONIC VEHICLES... 634 Q. Lu, H. Han, L. Hu, J. Yu INVESTIGATION OF DIVERT CONTROL JET INTERACTION EFFECTS ON AERODYNAMIC CHARACTERISTICS... 639 J. Fu, Y. Liu, Z. Ni, N. Cao STUDY OF GROUND TEST METHOD FOR NEAR SPACE PROPELLER... 646 X. Li, G. Li, B. Zhou, W. Zhu, K. Sun ANALYSIS AND SIMULATION OF FC-1553B DOUBLE-STAR NETWORK IN AVIONICS SYSTEM... 652 X. Zhu, H. Zhou, F. Zhang, X. Yang APPLICATION OF AEKF PARAMETER IDENTIFICATION TO UAV AUTOPILOT... 665 Z. Liu, G. Wang, Y. Zhou A PROBABILISTIC APPROACH TO AIRCRAFT ARRIVAL SEQUENCING AND CONFLICT RESOLUTION... 673 Y. Matsuno, T. Tsuchiya IN-PLANE MECHANICAL PROPERTIES OF INTEGRATED SKINS... 681 L. Chang, X. Shen, J. Wang A COMPARATIVE STUDY OF ROAD EXTRACTION TECHNIQUES FROM AERIAL IMAGERY A NAVIGATIONAL PERSPECTIVE... 692 A. Volkova, P. Gibbens UNSTEADY QUASI-ONE-DIMENSIONAL MODELLING FOR PROPULSION SYSTEMS... 710 C. Doolan Author Index