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Theoretical and Experimental Investigation of Geomagnetic Energy Effect for LEO Debris Deorbiting 期刊论文
AEROSPACE, 2022, 卷号: 9, 页码: 511
作者:  Feng GH(冯冠华);  Zhang C(张晨);  Zhang H(张珩);  Li WH(李文皓)
Adobe PDF(14157Kb)  |  收藏  |  浏览/下载：123/34  |  提交时间：2022/10/23
LEO debris deorbiting  geomagnetic energy (GME) propellant  ground proof-of-principle experiment  LEO GME utilization  
Geomagnetic Energy Approach to Space Debris Deorbiting in a Low Earth Orbit 期刊论文
INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2019, 页码: AR5876861
作者:  Feng GH(冯冠华);  Li WH(李文皓);  Zhang H(张珩)
Adobe PDF(4813Kb)  |  收藏  |  浏览/下载：479/78  |  提交时间：2019/04/11
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
作者:  Feng GH(冯冠华);  Li WH(李文皓);  Zhang H(张珩)
Adobe PDF(743Kb)  |  收藏  |  浏览/下载：372/81  |  提交时间：2018/12/28
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
作者:  Zhang J(张杰);  Zhang H(张珩);  Xiao XX(肖歆昕)
Adobe PDF(4293Kb)  |  收藏  |  浏览/下载：287/85  |  提交时间：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
作者:  Feng GH(冯冠华);  Li WH(李文皓);  Zhang H(张珩)
Adobe PDF(1780Kb)  |  收藏  |  浏览/下载：250/65  |  提交时间：2018/10/29
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
作者:  Feng GH;  Li WH(李文皓);  Zhang H(张珩);  Xiao XX(肖歆昕);  Zhang J(章杰)
浏览  |  Adobe PDF(249Kb)  |  收藏  |  浏览/下载：354/82  |  提交时间：2018/06/06
Probability Distribution Evolution Algorithm (Pde)  Inertial Parameters Identification  Space Target  Pseudo-inverse Solution Consistency  
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
作者:  Li WH(李文皓);  Xiao XX(肖歆昕);  Zhang H(张珩);  Xiao XX(肖歆昕)
浏览  |  Adobe PDF(1066Kb)  |  收藏  |  浏览/下载：414/90  |  提交时间：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  
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
作者:  Zhang H(张珩);  Xu B(许滨);  Zhang ZM
浏览  |  Adobe PDF(248Kb)  |  收藏  |  浏览/下载：147/48  |  提交时间：2017/06/01
Analytical Approach  Flight Trajectory  Formation Flying  Reference Spacecraft  Relative Motion  Simplified Formula  
微机虚拟现实(PCVR)应用相似论研究探讨/Study on similarity theory application to PCVR 会议论文
3rd World Congress on Intelligent Control and Automation, HEFEI, PEOPLES R CHINA, JUN 28-JUL 02, 2000
作者:  齐曼;  张珩;  Zhang GJ;  Qi JH;  Qi, M (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
浏览  |  Adobe PDF(314Kb)  |  收藏  |  浏览/下载：103/34  |  提交时间：2016/06/30