中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
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The Digital Assembly and Maintenance Training Platform for ITER-Type Mock-Up in Virtual Reality Environment 期刊论文  OAI收割
FUSION SCIENCE AND TECHNOLOGY, 2021, 页码: 10
作者:  
Li, Jin-Yang;  Guo, Sheng-Miao;  Gu, Long;  Zhang, You-Peng;  Yang, Sheng
  |  收藏  |  浏览/下载:30/0  |  提交时间:2021/12/09
Design and synthesis of further simplified pyripyropene A based ACAT2 selective inhibitors 期刊论文  OAI收割
TETRAHEDRON, 2019, 卷号: 75, 期号: 12, 页码: 1819-1825
作者:  
Liu, Yi;  Zhang, Xiaowei;  Zhan, Yang;  Li, Boliang;  Lu, Wei
  |  收藏  |  浏览/下载:14/0  |  提交时间:2020/07/01
Design of a miniature axial flux flywheel motor with PCB winding for nanosatellites (EI CONFERENCE) 会议论文  OAI收割
2012 International Conference on Optoelectronics and Microelectronics, ICOM 2012, August 23, 2012 - August 25, 2012, Changchun, China
Wu J.
收藏  |  浏览/下载:40/0  |  提交时间:2013/03/25
This paper presents the design and analysis of an axial flux permanent-magnet (AFPM) machine for nanosatellites application. It is a miniature axial flux surface mounted permanent magnet flywheel motor  using a printed circuit board (PCB) stator winding. The PCB stator has simplified the design and construction and avoids unnecessary space  since size reduction has become one of the most important aspects of flywheel motor design for nanosatellites. The performances of the machine are estimated by combination method of three-dimensional (3D) electromagnetic finite element analysis (FEA) and approximate theoretical analysis. The back EMF and electromagnetic torque are derived. A comparison between the analysis and experimental measurement results of the prototype machine is also presented. Both simulated and experimental results show that the proposed motor would be an acceptable solution for the nanosatellite applications with advantages such as simple structure and low-cost  as multi-layer circuit board production techniques have made the production of printed circuit coils cheaper and easier. 2012 IEEE.  
Adaptive control at launching using three loop autopilot (EI CONFERENCE) 会议论文  OAI收割
2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China
作者:  
Zhang Y.
收藏  |  浏览/下载:25/0  |  提交时间:2013/03/25
In order to guarantee the precise initial flight trajectory  control the missile disturbance of large disturbance torque  three loop adaptive autopilot was researched. The characteristics of the projectile and three loop autopilot instruction formation characteristics were analysed. From equivalent pitching angle of lateral acceleration feedback loop  combined with the instruction of generalized error  autopilot structure was simplified  and three loop autopilot adaptive control law and stability were designed. The test data show that when disturbance torque was 600Nm  the attitude angle generalized error was -4.4. In the time lasted about 15s  late trajectory accuracy was within 1.0.Three loop autopilot adaptive control law was able to control the disturbance of initial trajectory and adapt to dynamic characteristics changes  control system stability. It was the initial trajectory accurate solution method of flight. 2011 IEEE.  
Design of control system of DC motor based on fusion FPGA (EI CONFERENCE) 会议论文  OAI收割
2011 International Conference on Mechatronics and Materials Processing, ICMMP 2011, November 18, 2011 - November 20, 2011, Guangzhou, China
Zhu D. D.; Li H. W.
收藏  |  浏览/下载:34/0  |  提交时间:2013/03/25