V423,Spacecraft design and construction of

About 112 item dissertation in line with V423,Spacecraft design and construction of query results,the following is 1 to 50(Search took 0.036 seconds)

Analysis of Space Capsule Water and Landing Impact Compatibility,WangYuXiang/Tsinghua University,0/10
The General Optimization Design of Small Satellites Based on Cloud Model,ChenChangChun/Harbin Institute of Technology,0/138
Research on Method of Thermal Design and Analysis of Spaceborne Mechanism with Sinda and TMG,SongHuiKai/Harbin Institute of Technology,0/36
Research on Design and Optimization of Capture and Docking System for Space Cooperative Object,DuZuo/Harbin Institute of Technology,0/30
Research on Active Lubrication Oriented Piezoelectric Micro-jet Generator for Spacecraft,LengYue/Harbin Institute of Technology,0/26
Linear Simulation Technology Research about Nonlinear Problems of Space Agencies,HeShuai/Graduate Schoo,Chinese Academy of Sciences,0/0
The high overload condition of ball screw failure analysis and Experimental Research on Performance,XuLingLing/Nanjing University of Technology and Engineering,0/23
Experimental Studies on the Friction Torque of Ball Bearing Used in Space Mechanism under Several Lubrication Conditions,YuanDingXin/Harbin Institute of Technology,0/47
Research on Low Shock and Large Load Hold-down/Release Mechanism Based on Shape Memory Alloy,JiangJinMin/Harbin Institute of Technology,0/75
Study on Collaborative Optimization Design of Satellite Constellation,ChangHui/Huazhong University of Science and Technology,0/1
Research on Energy Absorbers of Legged-type Lander and Dynamic Simulation on Its Soft Landing Process,LiMeng/Harbin Institute of Technology,0/1
Design and Implement of Integrated Services Unit for Satellitic Electronic System,SongZhiCheng/Xi'an University of Electronic Science and Technology,0/8
The analysis of contact characteristics of ball screw friction efficiency and space conditions,CaoZuo/Nanjing University of Technology and Engineering,0/88
Study on Solar Array Wing of Spacecraft with Deployment by Step,ZhangLei/Shanghai Jiaotong University,0/107
Research on the Key Technology of Stealth Micro Satellite Structure Design,ZhengZuo/Nanjing University of Aeronautics and Astronautics,0/352
Study on analysis method of modern small satellite reliability,ZhangPeng/Harbin Engineering University,1/164
Research on Key Issues of Knowledge Sharing for Aerospace Product in Product Development,YuDeHai/Chongqing University,1/201
Mechanism Theory Research of5-DOF Adjusting Parallel Platform,PanQiuYue/Yanshan University,0/8
Design and research of aerospace precision gear planetary roller screw,GaoLiang/Nanjing University of Technology and Engineering,0/181
Investigations on Running Characteristics of the Mechanically Pumped Cooling Loop for Space Applications,LiuJie/Shanghai Jiaotong University,0/400
Study on Integrated Design Optimization of Satellite Constellation,FanLi/National University of Defense Science and Technology,6/632
Reverse Design of the Space Deployable Antenna and Study on Stowing of the Space Structure,ShouJianJun/Zhejiang University,2/783
Bi-system Co-evolutionary Algorithm and Key Techniques of the CAD System for Satellite Module Layout,ZengWei/Dalian University of Technology,5/289
Particle Swarm Optimization Algorithm for Satellite Module Layout Optimization,ZhangBao/Dalian University of Technology,1/483
Thermal Control Shutter System Design of XX Sencondary Satellite and Collaborative Simulation of Virtual Prototyping,LaiYiZuo/Harbin University of Science and Technology,2/474
The Cooperative Co-Evolutionary Differential Evolution and Its Applications for Complex Layout Optimization,ShiYanJun/Dalian University of Technology,8/478
Sequential and Physical Decomposition Methods for a Layout Design Problem of Spacecraft,SunZhiGuo/Dalian University of Technology,4/489
Distributed Coevolutionary Multidisciplinary Design Optimization Methods for Flying Vehicles,ChenZuoFeng/People's Liberation Army National Defense University of Science and Technology,60/1763
Human-Computer Interactive Evolutionary Design Method and Its Application to Spacecraft Vessel Layout Scheme Design,QianZhiQin/Dalian University of Technology,20/644
Study on the Mechanism and Passive/Active Control Methods of the Dynamic Stability of the Reentry Capsules,ZhaoHaiYang/National University of Defense Science and Technology,4/130
Study on the Theory and Application of Multidisciplinary Design Optimization for the Satellite System,ZhaoYong/National University of Defense Science and Technology,4/767
Research on the Intelligent Computational Methods for the Layout Optimization Problems in Satellite Capsule,XuYiChun/Huazhong University of Science and Technology,1/223
Study on Several Graphic Problems for Satellite Module Layout,LiZiQiang/Dalian University of Technology,2/233
Satellite Constellation Design Based on Genetic Algorithm,ZengYuJiang/Huazhong University of Science and Technology,4/778
Satellite Payloads Configuration and Layout Design Method,WangZuoShou/Dalian University of Technology,1/611
Simulation of the Ventilation in Manned Spacecraft Cabin and Weight Reduction Analysis,LiangZhen/Harbin Institute of Technology,3/284
Research on Key Technology of Tribology System of the Attitude Control Flywheel,HuangDunXin/Graduate Schoo,Chinese Academy of Sciences,0/190
Numercial Simulation and Thermal Control Chararistic of the Space Mechanically Pumped Two-Phase CO₂ Loop,HuangZhenCheng/Sun Yat-sen University,0/136
Human Computer Cooperative Evolutionary Design Based on Distribution Estimation,LiuJun/Dalian University of Technology,0/192
Computational Methods of Non-proportionally Damped Structures with Applications to Satellite Design,LiuMingHui/Harbin Institute of Technology,4/112
Multi-performance Optimization of Structures and Its Application in Aerospace Structural Design,WangBin/Dalian University of Technology,6/360
The Distributed Satellite interferometer track design,XuAiMin/PLA Information Engineering University,0/51
Algorithm and Implementation of the high - bit-rate QPSK demodulator carrier recovery loop,HongZhenHong/Graduate School, Chinese Academy of Sciences,3/524
Design and Study on Controller in the Moment Wheel System Suspended by Active Magnetic Bearings,ZhangXiao/Tsinghua University,0/142
Design and Implementation of GPS L1 Pseudolite Signal Generator,LiuZuoZhi/Shanghai Jiaotong University,0/228
A Study of Arithmetic for Automatic Antenna Track of Satellite,SunXingBang/Dalian Maritime University,9/339
The Study & Application on Sensors of Inmarsat SES Tracing Antenna System,WuHouDe/Dalian Maritime University,3/170
Miniature spacecraft detection system and its Target Recognition Algorithm,LiuHui/Xi'an Optics and Fine Mechanics,0/254
Optimization Design and Its Application Analysis of a Constellation with Common Ground Track,BaoHaiTao/Huazhong University of Science and Technology,1/205
Multi-objective Dual-system Co-Evolutionary Algorithm and Its Application,LiCan/Dalian University of Technology,1/280