机构

• 长春光学精密机械与物... [2]
• 自动化研究所 [1]
• 沈阳自动化研究所 [1]

采集方式

• OAI收割 [4]

内容类型

• 会议论文 [3]
• 期刊论文 [1]

发表日期

• 2016 [1]
• 2015 [1]
• 2011 [1]
• 2010 [1]

学科主题

筛选

浏览/检索结果: 共4条，第1-4条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 Research on the Temperature Control Methods to a Hemodialysis System with Large Inertia and Hysteresis 会议论文  OAI收割 35th Chinese Control Conference (CCC), Chengdu, China, 2016年7月27-29日 作者:  Lan S(兰盛);  Li En（李恩）;  Liang Zize（梁自泽）;  LAN Sheng 收藏  |  浏览/下载：31/0  |  提交时间：2017/05/05 Hemodialysis  Large Inertia  Hysteresis  Temperature Control   Load equivalent simulation method of ultra-large moment of inertia of space station redocking manipulator 期刊论文  OAI收割 Journal of Information and Computational Science, 2015, 卷号: 12, 期号: 2, 页码: 431-441 作者:  Xu ZG(徐志刚);  Bai XL(白鑫林);  Yang MY(杨明毅);  Wang JY(王军义) 收藏  |  浏览/下载：39/0  |  提交时间：2015/03/17 Space Station Redocking Manipulator  Ultra-large Moment of Inertia Simulation  Equivalent Dynamics  Equivalent Moment of Inertia   Study on the servo system of large telescope based on the internal model pid control strategy (EI CONFERENCE) 会议论文  OAI收割 IEEE 2011 10th International Conference on Electronic Measurement and Instruments, ICEMI 2011, August 16, 2011 - August 18, 2011, Chengdu, China Li H. 收藏  |  浏览/下载：21/0  |  提交时间：2013/03/25 This paper developed the internal model PID control for large telescope control system considerations in more parameters adjustment in servo control loop at present. The large electro-optic telescope system belongs to a big inertia system. This simplifies the debug process  the feasibility and robustability are also verified by the analyses and simulation results that satisfy the high precision demand. The practicability of this algorithm is verified in an actual project that only two parameters need adjusted. The application shows that this system runs stably with high accuracy. The technology and methods adopted in the system are practical and worthy of using abroad. 2011 IEEE.   Analysis of inertia dyadic uncertainty for small agile satellite with control moment gyros (EI CONFERENCE) 会议论文  OAI收割 2010 IEEE International Conference on Mechatronics and Automation, ICMA 2010, August 4, 2010 - August 7, 2010, Xi'an, China 作者:  Zhang L.;  Zhang L.;  Sun Z. 收藏  |  浏览/下载：20/0  |  提交时间：2013/03/25 With the increasing demands for the agility of the next earth imaging satellite  control moment gyro (CMG) is considered to be the most suitable actuator because of its torque amplification capability. However  a CMG system may introduce uncertainty of inertia dyadic to a satellite's attitude control system. The uncertainty is negligible for large space vehicles  but it has not been tested whether it can be ignored for small agile satellites. How to model the CMG system inertia dyadic varying with gimbal angles  and what influence it will put on the performance of attitude control system haven't been test accurately as well. All of them are dealt with mathematically and accurately in this paper. This paper firstly gives mathematic descriptions of the inertia dyadic of the 4-CMG pyramid configuration system  varying with gimbal angles  and then designs a variable structure control law for small agile satellite using CMGs. Finally  numerical simulation suggests that the inertia dyadic variation of a 4-CMG pyramid configuration system is approximately centesimal of the total inertia dyadic of the satellite  and that the designed variable structure control law is of good robust performance for an example of large-angle attitude maneuver  despite of the variation of the inertia dyadic. 2010 IEEE.