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| A continuous contact force model for impact analysis in multibody dynamics 期刊论文
MECHANISM AND MACHINE THEORY, 2020, 卷号: 153, 页码: 25
作者: Zhang J; Li WH(李文皓) ; Zhao L; He GP
 Adobe PDF(5467Kb) |  收藏 | 浏览/下载：1464/1223 | 提交时间：2020/11/30
Contact force model Energy loss Complex geometries Multibody dynamics |
| Development of a Wheeled and Wall-pressing Type In-Pipe Robot for Water Pipelines Cleaning and its Traveling Capability 期刊论文
MECHANIKA, 2020, 卷号: 26, 期号: 2, 页码: 134-145
作者: Feng GH(冯冠华); Li WH(李文皓); Li ZQ; He Z
Adobe PDF(844Kb) | 收藏 | 浏览/下载：248/82 | 提交时间：2020/08/26
wheeled and wall-pressing type in-pipe cleaning robot (IPCR) preload mechanism traction force obstacle-overcoming capability simplified vibration system |
| 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)
 浏览 | Adobe PDF(4813Kb) | 收藏 | 浏览/下载：480/78 | 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)
浏览 | Adobe PDF(743Kb) | 收藏 | 浏览/下载：372/81 | 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)
浏览 | Adobe PDF(1780Kb) | 收藏 | 浏览/下载：251/65 | 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：356/82 | 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：415/90 | 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 |
