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浏览/检索结果: 共20条，第1-10条 帮助

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Piecewise Linear Weighted Iterative Algorithm for Beam Alignment in Scanning Beam Interference Lithography 期刊论文  OAI收割
Photonic Sensors, 2019, 卷号: 9, 期号: 4, 页码: 344-355
作者:  Y.Song;  Bayanheshig;  S.Li;  S.Jiang;  W.Wang
  |  收藏  |  浏览/下载：33/0  |  提交时间：2020/08/24
CFD-DEM modeling the effect of column size and bed height on minimum fluidization velocity in micro fluidized beds with Geldart B particles 期刊论文  OAI收割
POWDER TECHNOLOGY, 2017, 卷号: 318, 页码: 321-328
作者:  Xu, Yupeng;  Li, Tingwen;  Musser, Jordan;  Liu, Xiaoxing;  Xu, Guangwen
  |  收藏  |  浏览/下载：27/0  |  提交时间：2017/11/27
Tuning of Ionic Interaction and Rheological Properties of Nanoscale Ionic Materials 期刊论文  OAI收割
CHEMICAL JOURNAL OF CHINESE UNIVERSITIES-CHINESE, 2016, 卷号: 37, 期号: 4, 页码: 767-774
作者:  Liu Yangjian;  Ruan Yingbo;  Zhang Baoqing;  Qiao Xin;  Liu Chenyang
收藏  |  浏览/下载：27/0  |  提交时间：2017/01/23
A Proportional-Feedforward Position Controller Based on Tracking-differentiator of PMSM 会议论文  OAI收割
World Congress on Intelligent Control and Automation, Guilin, 2016.06
作者:  Hao Lu;  Jianhua Hu;  Yunkuan Wang;  Jun Zheng;  Xiaofei Qin
收藏  |  浏览/下载：48/0  |  提交时间：2016/10/21
PMT overshoot study for the JUNO prototype detector 期刊论文  OAI收割
CHINESE PHYSICS C, 2016, 卷号: 40, 期号: 9
作者:  Liao DH(廖东豪);  Xu MH(徐美航);  Qin ZH(秦中华);  Wang PL(王佩良);  Wang ZM(王志民)
  |  收藏  |  浏览/下载：34/0  |  提交时间：2017/07/27
PMT overshoot study for the JUNO prototype detector 期刊论文  OAI收割
CHINESE PHYSICS C, 2016, 卷号: 40, 期号: 9
作者:  Luo, Feng-Jiao;  Heng, Yue-Kun;  Wang, Zhi-Min;  Wang, Pei-Liang;  Qin, Zhong-Hua
  |  收藏  |  浏览/下载：17/0  |  提交时间：2023/03/16
Origin of stress overshoot in amorphous solids 期刊论文  OAI收割
MECHANICS OF MATERIALS, 2015, 卷号: 81, 页码: 72-83
作者:  Jiang, MQ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.;  Jiang MQ(蒋敏强);  Wilde G;  Dai LH(戴兰宏)
  |  收藏  |  浏览/下载：31/0  |  提交时间：2015/03/17
Molecular Mechanisms for Conformational and Rheological Responses of Entangled Polymer Melts to Startup Shear 期刊论文  OAI收割
macromolecules, 2015, 卷号: 48, 期号: 12, 页码: 4164-4173
作者:  Lu,Yuyuan;  An,Lijia;  Wang,Shi-Qing;  Wang,Zhen-Gang
收藏  |  浏览/下载：31/0  |  提交时间：2016/05/06
LABTM control system based on FPGA (EI CONFERENCE) 会议论文  OAI收割
2nd International Conference on Mechatronics and Applied Mechanics, ICMAM 2012, December 8, 2012 - December 9, 2012, Taiwan
作者:  Wang Y.;  Yu P.;  Yu P.;  Wang Y.;  Wang Y.
收藏  |  浏览/下载：153/0  |  提交时间：2013/03/25
This paper presents the digital PI control method for design and simulation of a high precision limited angle brushless torque motor control system in Field Programmable Gate Array device (FPGA). The direct drive structures which are widely applied in many servo control fields. Matlab Xilinx System GeneratorR toolbox based on Fixed-Point Arithmetic is used to design the digital PI controller using DSP architecture  plot the responses of the control system and generate the VHDL source code. The control system model consists of a digital PI  a real LABTM  and a real absolute Inductosyn  encoder to rpm and position blocks. Through loading generated codes in process of the simulation that built by the digital discrete model  it is verified that the rising time of current loop is only 1.2ms  and rate loop is 8ms  overshoot is rarely 4.2%. Finally  the comprehensive positioning accuracy of system can reach up to 5 arc sec  and the rate jitter achieves 5% with the 4 arc sec accuracy absolute Inductosyn. (2013) Trans Tech Publications  Switzerland.  
The aircraft autopilot design of parameters changing in a wide range (EI CONFERENCE) 会议论文  OAI收割
2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, April 15, 2011 - April 17, 2011, Wuhan, China
Zhen D.; Yue Z.
收藏  |  浏览/下载：28/0  |  提交时间：2013/03/25
Autopilot is an important part of aircraft  Under the action of the disturbance torque  for the flight parameters of aircraft Changing in a wide range  the range was about 16km  on the basic of analyzing the typical trajectory  the max height was about 5100m  the trajectory of feature points were selected  the deviation of lateral was about 12m  taking pitch control loop for example  the maximum angle of attack was about 3.6  a sub- PID autopilot was designed using classical control theory  the maximum elevator deflection was less than 5  using single-mode Transient suppression method  the maximum aileron deflection was less than 2  the overload due to control surface transition deflection was avoided when control parameters changing  the maximum roll was less than 5  the verification was done by non-linear simulation. The result showed that: the phase margin of autopilot was greater than 30  the response of overload can accurately track the given overload instruction. An autopilot design method of aircraft of parameter changes in a wide range was provided. 2011 IEEE.  the bandwidth was more than 14rad / s  the settling time was less than 0.7s  the maximum overshoot was 23.3%