About 6962 item dissertation in line with V2,Aviation query results,the following is 1 to 50(Search took 0.016 seconds)

  1. Research of Unmanned Quadrotor Based on Intelligent Control,LiZeGuo/Tianjin University of Science and Technology,0/64
  2. Pyramid Angle Measurement Methods of Helicopter Rotor Blades,JiangMai/Harbin Engineering University,0/14
  3. Research on Key Problems of Dynamics of Helicopter Tail-Drive Transmission System,ZhuZiBing/Nanjing University of Aeronautics and Astronautics,0/40
  4. The Embedded System for Intelligent Video Monitoring in UAV,HuangWeiJie/Shenyang University,0/52
  5. Study and Design on Wave-off Decision System of Carrier-based Airplane,TangYunFeng/Northeastern University,0/8
  6. Vision-Based Fast SLAM for Small Scale Unmanned Helicopter,HeYing/Harbin Institute of Technology,0/21
  7. Three-dimensional Initial form Analysis of Inflated Wing,CuiYuJia/Harbin Institute of Technology,0/20
  8. Structural Design and Numerical Aeroelastic Analysis of Airship Envelope,YangLiuYi/Harbin Institute of Technology,0/67
  9. The Research of Measurement and Calibration on the Flapping Parameters of Rotor Blades,ShaoChongZuo/Harbin Institute of Technology,0/20
  10. Robust Flight Controller Design for Model-scale Helicopters Via Parametric Approach,ZhouZhiGang/Harbin Institute of Technology,0/38
  11. Optimization Design of Engine Support System of Small UAV,XingXiangLiang/Graduate Schoo,Chinese Academy of Sciences,0/19
  12. Structure Optimization of the Main Frame Made of Composite Material in the Pint-size UAV,XuXiaoChen/Graduate Schoo,Chinese Academy of Sciences,0/33
  13. 3-Dimensional UAV Path Planning Based on Improved Particle Swarm Optimization Algorithm,WangWenZuo/Shenyang University of construction,0/16
  14. Stroboscopic Visualization Information Extraction of Hovering Micro Air Vehicle Prototype with Flexible Aerodynamic Shape under Airflow Disturbance,ZhangNingNing/Tianjin University,0/2
  15. Research on STOVL Aircraft Thrust Nozzle,HongLiang/Nanjing University of Aeronautics and Astronautics,0/10
  16. Research on the Helicopter's Fuel Tank Crashworthiness Based on the Fluid-solid Coupling,ZhangHaiHua/Harbin Engineering University,0/27
  17. Numerical Simulation and Model Design of More Than Two Flapping-wings Micro Air Vehicle,HeYaNan/Harbin Institute of Technology,0/46
  18. Reserch on Optimal Controller Design for UAV,ZhongBin/Nanchang University of Aeronautics and,0/46
  19. Localization for Quadrotor Unmaned Aerial Vehicle in Complex Environment,GuoFang/Tianjin University,0/7
  20. Simulation Analysis for Vibration of Tail Drive System and Fuselage under Maneuvering State,LiuJinJin/Nanjing University of Aeronautics and Astronautics,0/16
  21. The Thermal Analysis of Helicopter Main Reducer Based on Thermal Network Method,YangPan/Nanjing University of Aeronautics and Astronautics,0/14
  22. Research on Visual Guided UAV Landing Technology Based on the Combination of Visual Features and Cooperative Object Optimization,WangXiaoHong/Nanjing University of Aeronautics and Astronautics,0/18
  23. Research on Vision-based for Landmark Tarcking and Landing of Unmanned Helicopter,YuCheng/Harbin Engineering University,0/40
  24. The Rcsearch on Vision-based Small Unmanned Helicopter Autonomous Landing,ChenDiShi/Zhejiang University,0/14
  25. Mechanics Analysis and Optimal Design of Key Bulkheads in UAV,DuQiXiang/Zhejiang University,0/17
  26. Airworthiness Compliance Approach of Fatigue Assessment for the Modification Design of Helicopter,ZhangTao/Nanjing University of Aeronautics and Astronautics,0/8
  27. Research for Dual Redundancy Electromechanical Actuation System of UAV Landing Gear,LiZuo/Nanjing University of Aeronautics and Astronautics,0/13
  28. Study on Evaluation Methods of Chief Performance Parameters for Helicopter Main Reducer,QiuJiang/Nanjing University of Aeronautics and Astronautics,0/29
  29. Research on Task Allocation&Attack Effectiveness Evaluation Technique for UAVs Cooperatively Combating,ChengCong/Nanjing University of Aeronautics and Astronautics,0/63
  30. Research on Nonliner-dynamic Modeling Technology for Unmanned Helicopter,HuangXianKai/Nanjing University of Aeronautics and Astronautics,0/20
  31. Research on Air-to-ground Reconnaissance Mission Planning System of UAV,TongYingFei/Nanjing University of Aeronautics and Astronautics,0/29
  32. Research of UAV Fault Injection and Diagnosis Real-time Simulation Platform Based on VxWorks,HuaLiangHao/Nanjing University of Aeronautics and Astronautics,0/20
  33. Optimization Technology Research on the Stabie Structure of Aviation Pods,ZuoLiJun/Changchun University of Science and Technology,0/6
  34. Route Planning for Unmanned Aerial Vehicles Based on Cloud Model,HanXu/Changchun University of Science and Technology,0/2
  35. Research on the Structure of Small Opto-electronic Stabilized Platform Assembled on UAV,LiZuo/Changchun University of Science and Technology,0/1
  36. Research of Airship Simulator Platform Control Technique,ZhaoJiaYun/Changchun University of Science and Technology,0/1
  37. Thrust Vector Modeling of Engine and Maneuvering Control of Advanced Fighter Aircraft,HuTianWen/Nanjing University of Aeronautics and Astronautics,0/16
  38. Design of Wireless Sensor Network in the Giant Airship Volume Measurement System,OuYangZhiWei/Hunan University,0/10
  39. Several Key Technological Research of Change Detection of Remote Sensing Images Base on Unmanned Aircraft,LiWei/Jimei University,0/73
  40. Research on Intelligent Control Algorithm for UAV Three-axis Self-stable Pan-tilt,GuoBingKun/Jimei University,0/118
  41. The Mini Unmanned Helicopter Based on Embedded Linux Real-time Positioning,YangXiaoFeng/Anhui University of Technology,0/11
  42. Parametric Sensitivity Analysis and Optimization for Nonrigid Airship,LuZhengZheng/Harbin Institute of Technology,0/45
  43. Research of the Motor Drive System in Four Rotor Unmanned Aerial Vehicle (UAV),LiuYang/Nanchang University of Aeronautics and,0/87
  44. Research on Pre-deformation for High-aspect-ratio Wing of UAV,XuJiangFeng/Nanchang University of Aeronautics and,0/65
  45. Research on Flapping-wing Flight Principle and Mechanism of the Imitating Butterfly Ornithopter,LeiYaChao/Nanchang University of Aeronautics and,0/110
  46. The Analysis of Static Strength for an Unmanned Aerial Vehicle,WangXu/Nanchang University of Aeronautics and,0/74
  47. Analysis of Static Strength for an UAV'S Wing,FengLiHua/Nanchang University of Aeronautics and,0/83
  48. Research on Ground Remote Telemetry System of Unmanned Aerial Vehicle,MaZuo/Nanchang University of Aeronautics and,0/156
  49. Structural and Strength Analysis of the Tilt-ducted UAV,DaiLiangZhong/Nanchang University of Aeronautics and,0/42
  50. Quick Failure Data Retrieval System of Unmanned Aeral Vehicle,JiaMuZi/Changchun University of Science and Technology,0/1

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