Aircraft design - Dissertation

About 1562 item dissertation in line with Aircraft design query results,the following is 1 to 50(Search took 0.025 seconds)

Study of Photogrammetric Technique for Center of Mass Determination,XiangZhengWei/Harbin Institute of Technology,0/33
Dynamic Modeling and Control for Parallel Polishing Manipulator,WeiWen/Harbin Institute of Technology,0/37
On the Trajectory Planning and Trajectory Tracking Control of Free-floating Space Robot,DaZuo/Harbin Institute of Technology,0/53
Impact/Contact Dynamic Modeling and Simulation of Space Robotic Manipulator for On-orbit Servicing,WuXiaoJian/Nanjing University of Aeronautics and Astronautics,0/16
A Study on Bearing-only Multi-target Location Based on Data Fusion,MaoGuanLiHua/Zhejiang University,0/21
The Numerical Simulation of the Cold Flow Properties in the Advanced Vortex Combustor,TuGuoHui/Nanchang University of Aeronautics and,0/25
Research on Automation Control and Intelligent Management of Air-condition System for XXX Project,ChenTieSheng/Harbin Institute of Technology,0/83
Study on Analysis of Aircraft Carrier's Attitude Motion,WeiJiaQing/Harbin Institute of Technology,0/53
Research on Terminal Guidance and Control of Interception for Maneuvering Targets,LiuZhiGao/Harbin Institute of Technology,0/35
Research on Technology of Initial Alignment and Inertial Device Calibration off the Lunar Surface,WangSi/Harbin Institute of Technology,0/42
Study on Maneuvering Penetration, Guidance and Control Problems for Ballistic Missile,WeiPengZuo/Harbin Institute of Technology,0/176
Research on Load Environmental Prediction for Missile Cabin Based on Energy Finite Element Analysis,LinYi/Harbin Institute of Technology,0/25
Research on Guidance Laws for Cooperative Attack of Multiple Anti-ship Missiles,ZhaoXueFeng/Harbin Institute of Technology,0/98
The Research of Gliding Phase Guidance for Hypersonic Glider Missile,LvRui/Harbin Institute of Technology,0/89
Design and Analysis of the Attack and Defense Ground Physical Simulation System,ShiZuo/Harbin Institute of Technology,0/10
Study on Autonomous Restoration of Navigation for Launch Vehicle During Active Phase,ZhongYongJian/Harbin Institute of Technology,0/13
Research on the Terminal Impact Angle Constraint Terminal Guidance Method of Anti-ship Missile,LeiZuo/Harbin Institute of Technology,0/68
Research on Trajectory Optimization and Design of Land-to-Land Ballistic Missile,LiZuo/Nanjing University of Aeronautics and Astronautics,0/25
The Analysis about Aerodynamic Performance and Structural Performance of Tapered Radome,LiangJiaZuo/Harbin Engineering University,0/14
The Study on Guidance and Control for Cooperative Engagement of Multi-missile,WuShengLiang/Nanjing University of Aeronautics and Astronautics,0/41
Study on Antimissile-cooperation Problems for Exo-atmospheric Multiple Kill Vehicle,MaYaBang/Harbin Institute of Technology,0/64
Numerical Simulation and Experimental of Supercavity of Mall Scale Projectile,GuoJianMing/Harbin Engineering University,0/24
Waverider Configuration Design、Optimization and Numerical Simulation of Aerospace Plane,YangYong/Harbin Institute of Technology,0/110
Launch Vehicle Fault-tolerant Navigation Filter and Applying Research,ShenDeFeng/Harbin Institute of Technology,0/39
Simulation and Analysis on Flight Dynamics for the Launch Vehicle's Ascent Stage,TangXiaoPing/Harbin Engineering University,0/69
Research for Launch Vehicle Flight Performence ANA Lyse and Evaluate Methods,WangZhen/Harbin Institute of Technology,0/28
Based on Hierarchical Neural Network Satellite Fault Diagnosis Technology Application Research,GaoYang/Harbin Institute of Technology,0/47
Dynamics Modeling and Deployment Control Research of Insar Satellite System,ZhangZhiGang/Harbin Institute of Technology,0/20
Research on Guidance and Control Algorithm for Softlanding of Deep Space Probe,YuWenJin/Harbin Institute of Technology,0/104
Reserch and Analysis on Iterative Guidance Self-adaptablility of Vehicle Base on Precise Control of Solution,LiWei/Harbin Institute of Technology,0/60
Study of Adaptive Terminal Guidance for Lifting Reentry Vehicle with Angular Constraint,LiangBiao/Harbin Institute of Technology,0/35
The Design of Satellite ACS Software Architecture and Key Component Based on Software Bus,ZuoRuiDong/Harbin Institute of Technology,0/41
Research on Adaptive Fault-tolerant Control System of Reusable Launch Vehicle,HanYu/Harbin Institute of Technology,0/27
Research on Fast Attitude Maneuver of Satellites Based on Flywheels and Thrusts,WuKai/Harbin Institute of Technology,0/66
Research on Fast Attitude Maneuver of Reconnaissance Satellites Based on Control Moment Gyros,SunXiangYu/Harbin Institute of Technology,0/55
Research on Sun Vector Determination Using Solar Panels Data,XingSiRui/Harbin Institute of Technology,0/25
Trajectory Optimization for Mars EDL and Research on the Entry Guidance,ZhouMeiJiang/Harbin Institute of Technology,1/0
Research on Attitude Detemination Algorithm of Fast Maneuver Satellites,LiYou/Harbin Institute of Technology,0/24
Research on Small Satellite Attitude Control by Fluid Momentum Loops,DanXiaoWei/Harbin Institute of Technology,0/25
Research on Satellite Attitude Control Based on Data-driven Theory,WangDongWei/Harbin Institute of Technology,0/23
Research on Architecture and Control Method of Spacecraft Formation,WangDongZhe/Harbin Institute of Technology,0/25
Robust Optimization and Stability Analysis of Spacecraft Dynamic Control Allocation,ZhaoYaFei/Harbin Institute of Technology,0/60
Transfer Trajectory Design and Analytical Predictor-corrector Entry Guidance Study for Manned Lunar Landing Mission,HuangRong/Harbin Institute of Technology,0/52
Research on Behavior-based Multi-behavior Control of Spacecraft Formation,SiJunTian/Harbin Institute of Technology,0/24
Study on Attitude Control Method of Heavy Launch Vehicle Based on Adaptive H_∞Control,ZhaoXiaoPing/Harbin Institute of Technology,0/20
The Dynamics and Control of Coulomb Satellite Formation,LiBoWen/Harbin Engineering University,0/24
Research on Omnidistance Maneuvering Guidance of Space-Based Reentry Vehicle,TangJunGang/Harbin Institute of Technology,0/112
Study on Autonomous Optical Navigation Technology for Deep Space Probe,LuRuiZuo/Nanjing University of Aeronautics and Astronautics,0/20
Numerical simulation of combustion process of non steady erosion of solid rocket motor,TangBiShun/Nanjing University of Technology and Engineering,0/20
Research on Transfer Trajectory Design Based on Three-body Model,FanZuo/Harbin Institute of Technology,0/35