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High Precision Loading Control Method for Sun-Tracking Unit Semi-physical Test System
会议论文
Edinburgh, United kingdom, July 16-19, 2019
作者:
Liu MY(刘明洋)
;
Xu ZG(徐志刚)
;
Zhao, Zhen
;
Bai XL(白鑫林)
;
Chen YL(陈月玲)
收藏
  |  
浏览/下载:27/0
  |  
提交时间:2019/12/14
sun-tracking unit
real-time system
nonlinear tracking-differentiator
semi-physical system
High Precision Loading Control Method for Sun-Tracking Unit Semi-physical Test System
会议论文
Edinburgh, United kingdom, July 16-19, 2019
作者:
Liu MY(刘明洋)
;
Xu ZG(徐志刚)
;
Zhao, Zhen
;
Bai XL(白鑫林)
;
Chen YL(陈月玲)
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/12/14
sun-tracking unit
real-time system
nonlinear tracking-differentiator
semi-physical system
Simulation Design of Space Target Tracking System based on Radial Motion Principle
会议论文
Nanjing, PEOPLES R CHINA, 2017-10-24
作者:
Yang, Yong-qing
;
Liu, Peng
;
Shen, Wen-ji
;
Han, Jun-feng
;
Liu, P (reprint author), Chinese Acad Sci, Xian Inst Opt & Precis Mech, Xian 710119, Shaanxi, Peoples R China.
收藏
  |  
浏览/下载:24/0
  |  
提交时间:2018/07/05
Radial Motion Principle
Space Target Tracking
In-orbit Test
Semi-physical Simulation
Effective Validation of the Semi-physical Test Bench for Sun Orientation
会议论文
7th Annual IEEE International Conference on Cyber Technology in Automation, Control, and Intelligent Systems (IEEE-CYBER 2017), Hawaii, USA, July 31 - August 4, 2017
作者:
Zhang X(张啸)
;
Xu ZG(徐志刚)
;
He Y(贺云)
;
Yin M(尹猛)
;
Zhang, Shixuan
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  |  
浏览/下载:30/0
  |  
提交时间:2017/12/21
Effective Validation
the Semi-physical Test Bench
Sun Orientation
Research on electromechanical resonance of two-axis tracking system
会议论文
2nd international conference on photonics and optical engineering, xi'an, china, 2016-10-14
作者:
Zhao, Zhi-Ming
;
Xue, Ying-Jie
;
Zeng, Shu-Qin
;
Li, Zhi-Guo
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  |  
浏览/下载:11/0
  |  
提交时间:2017/05/15
The Semi-physical Real-time Simulation and Test of IPMSM Considering the Iron Loss Effect
会议论文
2014 IEEE TRANSPORTATION ELECTRIFICATION CONFERENCE AND EXPO (ITEC) ASIA-PACIFIC 2014, 2014-08-31
作者:
Gao Jin[1]
;
Huang Yang[2]
;
Song Shiyang[3]
;
Huang Surong[4]
收藏
  |  
浏览/下载:8/0
  |  
提交时间:2019/04/30
digital virtual motor
iron loss
Hardware-in-loop
semi-physical real-time simulation
Implementation and Test for the Semi-physical Real-time Simulation of IPMSM Based on 3-D Inductance Table
会议论文
2014 IEEE TRANSPORTATION ELECTRIFICATION CONFERENCE AND EXPO (ITEC) ASIA-PACIFIC 2014, 2014-08-31
作者:
Gao Jin[1]
;
Song Shiyang[2]
;
Huang Yang[3]
;
Huang Surong[4]
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/04/30
Design of semi-physical simulation for small satellite by virtual display (EI CONFERENCE)
会议论文
2011 3rd International Conference on Mechanical and Electronics Engineering, ICMEE 2011, September 23, 2011 - September 25, 2011, Hefei, China
Xu K.
;
Lv Y.
;
Jin G.
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  |  
浏览/下载:19/0
  |  
提交时间:2013/03/25
Semi-physical simulation of attitude control system is the more synthetically test and verify for designing of small satellite control system. It is an important means of small satellite development. However
the results of current semi-physical simulation system have a lot of non-intuitive. Compare with the actual environment
the simulation environment still has striking disparity. So the shortcomings affect precision of simulation. Based on the virtual display technology
the group semi-physical simulation system has been constructed for attitude control of small satellite due to the combination with xPC real-time environment
the simulation computer
high-precision single-axis air-bearing turntable
reaction wheel
air thrust device
fiber gyroscopes
sensors synchronizer
power subsystem and wireless devices virtual display computer etc. Semi-physical simulation achieved the visual simulation in orbit and tracked new information of virtual environment of space into real-time simulation computer. Simulation results show that the simulation system for real-time attitude and orbit position of small satellite semi-physical simulation has an excellent display effect. At the same time
Real-time transfuse of orbit information provides a more accurate space environment simulation. The simulation system of small satellite attitude control to design and evaluate the more direct and convenient. (2012) Trans Tech Publications
Switzerland.
Semi-physical simulation of an optoelectronic tracking servo system based on C MEX S functions (EI CONFERENCE)
会议论文
2010 International Conference on Computer, Mechatronics, Control and Electronic Engineering, CMCE 2010, August 24, 2010 - August 26, 2010, Changchun, China
Juan C.
;
Junhong Z.
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  |  
浏览/下载:20/0
  |  
提交时间:2013/03/25
To the design of an optoelectronic tracking servo system
we test the method [1
not only the reasonability of the control algorithm should be considered
2]. The simulation results verify the theoretical analysis. Because C MEX S function has the features of fast execute speed
but the cost and time as well. It is necessary to establish the simulation model for the system. Applying the C MEX S functions
independently generated program
we can build the every independent digital control modules in MATLAB/SIMULINK for the optoelectronic tracking servo system. In the paper
directly download to the hardwires
we apply the C MEX S function to the design of the practical optoelectronic tracking servo system. For the speed
we can design and debug the digital control modules in MATLAB/SIMULINK and then transform and download directly to DSP processor. 2010 IEEE.
position loop control and TV delay compensations
基于结构奇异值的水下机器人鲁棒控制研究
会议论文
2010 8th World Congress on Intelligent Control and Automation (WCICA 2010), Jinan, China, July 7-9, 2010
作者:
刘开周
;
郭威
;
王晓辉
;
封锡盛
收藏
  |  
浏览/下载:27/0
  |  
提交时间:2012/06/06
载人潜水器
动力定位
鲁棒控制
混合灵敏度
结构奇异值
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