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Evaluation Method for Multi-Operator and Multi-Robot Teleoperation Systems 会议论文
2018 IEEE 3rd Advanced Information Technology, Electronic and Automation Control Conference (IAEAC), Chongqing, China, 12-14 Oct. 2018
Authors:  Feng GH(冯冠华);  Li WH(李文浩);  Zhang H(张珩)
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New Identification Method for Backlash of Gear Transmission Systems 会议论文
2nd IEEE Advanced Information Management,Communicates,Electronic and Automation Control Conference (IMCEC), Xi'an, China, 25-27 May 2018
Authors:  Zhang J(张杰);  Zhang H(张珩);  Xiao XX(肖歆昕)
View  |  Adobe PDF(4293Kb)  |  Favorite  |  View/Download:48/2  |  Submit date:2018/12/28
Space Robot Teleoperation Experiment and System Evaluation Method 会议论文
2018 2nd IEEE Advanced Information Management,Communicates,Electronic and Automation Control Conference (IMCEC), China, 25-27 May 2018
Authors:  Feng GH(冯冠华);  Li WH(李文皓);  Zhang H(张珩)
View  |  Adobe PDF(1780Kb)  |  Favorite  |  View/Download:47/3  |  Submit date:2018/10/29
Normal acceleration reduce guidanceand control for sub-orbit vehicle re-entry 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Li WH(李文皓);  Xiao XX(肖歆昕);  Zhang H(张珩);  Xiao XX(肖歆昕)
View  |  Adobe PDF(1066Kb)  |  Favorite  |  View/Download:116/21  |  Submit date:2018/01/16
Aerodynamics  Air Navigation  Angle Of Attack  Control Surfaces  Control Theory  Degrees Of Freedom (Mechanics)  Dynamic Models  Flight Control Systems  Flight Simulators  Monte Carlo Methods  Reentry  Spacecraft  Surface Reactions  Uncertainty Analysis  Vehicles  
Probability Distribution Evolution Algorithm to Inertial Parameters Identification for Space Target 会议论文
4th International Conference on Systems and Informatics (ICSAI), Hangzhou, PEOPLES R CHINA, NOV 11-13, 2017
Authors:  Feng GH;  Li WH(李文皓);  Zhang H(张珩);  Xiao XX(肖歆昕);  Zhang J(章杰)
View  |  Adobe PDF(249Kb)  |  Favorite  |  View/Download:101/13  |  Submit date:2018/06/06
Probability Distribution Evolution Algorithm (Pde)  Inertial Parameters Identification  Space Target  Pseudo-inverse Solution Consistency  
Improvement of the thermal design in the SiC PVT growth process 会议论文
7th International Workshop on Modeling in Crystal Growth, Taipei,TW, China, OCT 28-31, 2012
Authors:  Yan JY(颜君毅);  Chen QS(陈启生);  Jiang YN(姜燕妮);  Zhang H;  Chen, QS (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Micrograv, Beijing 100190, Peoples R China.
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Fluid Flows  Mass Transfer  Growth From Vapor  Semiconducting Silicon Compounds  
大气边缘超高速飞行的质量矩控制方法研究 会议论文
高超声速研讨会暨第五届全国高超声速科学技术会议, 中国广西桂林, 2012-11-12
Authors:  李文皓;  李帅辉;  刘洪伟;  张珩
View  |  Adobe PDF(61Kb)  |  Favorite  |  View/Download:514/77  |  Submit date:2014/03/19
大气层  直接力控制  气动力矩  控制律  飞行姿态  气动舵  控制方法  再入体  航天器  高超声速飞行  气动外形  边缘  机构设计  质心  舵面  Nelson  烧蚀  相对位移  控制领域  工质  
亚轨道飞行器再入攻角设计的法向过载动平衡方法 会议论文
第三届高超声速科技学术会议, 江苏·无锡
Authors:  李文皓;  肖歆昕;  张珩
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亚轨道飞行器再入通道概念及应用 会议论文
第三届高超声速科技学术会议, 江苏·无锡
Authors:  肖歆昕;  李文皓;  张珩
Adobe PDF(311Kb)  |  Favorite  |  View/Download:503/136  |  Submit date:2010/11/25
An analytical approach to analyzing spacecraft formation-flying motion 会议论文
AIAA Guidance, Navigation, and Control Conference and Exhibit 2002, Monterey, CA, United states, August 5, 2002 - August 8, 2002
Authors:  Zhang H(张珩);  Xu B(许滨);  Zhang ZM
View  |  Adobe PDF(248Kb)  |  Favorite  |  View/Download:10/4  |  Submit date:2017/06/01
Analytical Approach  Flight Trajectory  Formation Flying  Reference Spacecraft  Relative Motion  Simplified Formula