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Research on distributed cooperative optimisation control strategy for active distribution network based on combine-then-adapt diffusion algorithm 期刊论文
JOURNAL OF ENGINEERING-JOE, 2019, 期号: 16, 页码: 1911-1917
作者:  Wu, Lizhen;  Jiang, Libo;  Hao, Xiaohong
收藏  |  浏览/下载:0/0  |  提交时间:2022/03/01
Economic-driven FDI attack in electricity market 会议论文
作者:  Peng, Datian;  Dong, Jianmin;  Jian, Jianan;  Peng, Qinke;  Zeng, Bo
收藏  |  浏览/下载:6/0  |  提交时间:2019/11/26
Alleviation of post-contingency overloads by SOCP based corrective control considering TCSC and MTDC 期刊论文
IET GENERATION TRANSMISSION & DISTRIBUTION, 2018, 卷号: 12, 期号: 9
作者:  Bi, Ruyu;  Lin, Tao;  Chen, Rusi;  Ye, Jing;  Zhou, Xueming
收藏  |  浏览/下载:5/0  |  提交时间:2019/12/05
DC power transmission  thyristor applications  mathematical programming  minimisation  flexible AC transmission systems  failure analysis  power generation reliability  power transmission reliability  power generation scheduling  renewable energy sources  search problems  pattern clustering  load shedding  load flow  power transmission control  power generation control  post-contingency overload alleviation  SOCP based corrective control  TCSC  MTDC  high-voltage direct current device  flexible AC transmission system  smart grid  cascading failures  DC blocking  post-contingency corrective control  large-scale renewable energy generation integration  artificial intelligence optimisation-based method  second-order cone programming CC optimisation model  SOCP-based CC optimisation model  meshed AC-DC power systems  optimisation variables  OV  heuristic search method  sensitivity index  clustering algorithm  overloaded lines  thyristor controlled series capacitor compensation levels  multiterminal direct current power  load shedding minimisation  generation rescheduling minimisation  power flow equations  computational efficiency  IEEE 30-bus test system  line outage  
Study on supper resolution reconstruction based on staggered arrays (EI CONFERENCE) 会议论文
2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011, August 12, 2011 - August 14, 2011, Harbin, China
Yuan Z.; Xing Z.; Guang J.
收藏  |  浏览/下载:14/0  |  提交时间:2013/03/25
The image resolution can be improved without increasing the requirement to optical imaging systems' parameters and decreasing the size of CCD pixel by staggered arrays technology  which arranges several CCDs in a specific mode. In this paper  an image super resolution method of improving the image resolution for 1.5 times both in two directions by 4 linear arrays staggered based on this technology is presented  which avoids the large computation in a single time by use of circulation method. This method is proved effective by the digital simulation  and a simulated experiment platform is constructed to test its feasibility. The image resolution is improved for 1.42 times of the unreconstructed image according to the imaging experiment of resolution chart  which is closed to 1.5 times in ideal case. And also  the reconstructed and unreconstructed images are evaluated by the image information entropy  which proves that the reconstructed image contains more information. 2011 IEEE.  
Reuse-based SOC test integration and IEEE P1500 standard 期刊论文
2010, 2010
Wu Chao; Wang Hong; Yang Shi-yuan
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Small aircraft CAN bus signal acquisition equipment (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
Chen C.-Q.
收藏  |  浏览/下载:23/0  |  提交时间:2013/03/25
Small aircraft often used RS485 bus. But with the complexity of the small aircraft's subsystems increase and the progress of field bus technology  CAN bus systems in small aircraft use more and more widely. How to record real-time flight experiment data on the small aircraft's CAN bus and provide test data for reproducing the process of a small aircraft flying is very important. This paper presents a design method of signal acquisition device  it can be used for small aircraft flying field experiment. 2010 IEEE.  as the main chip with DSP2812  SJA1000 as CAN controller  CTM1050 as the CAN transceiver  CF card as storage media. Gives the diagram of its hardware and software design process. Combined with the background of a small aircraft  testing the instrument for data acquisition when the ground experiments and flight progress. Experimental data show that the design of high reliability and CAN signals can effectively complete the record  
Modular aircraft simulation platform based on simulink (EI CONFERENCE) 会议论文
2010 IEEE International Conference on Mechatronics and Automation, ICMA 2010, August 4, 2010 - August 7, 2010, Xi'an, China
Chen C.-Q.; Ji Y.
收藏  |  浏览/下载:19/0  |  提交时间:2013/03/25
Aircraft simulation platform is the most important supporting technology in the aircraft development process. This simulation platform can be used for validating the design of subsystem and also it provides the necessary data for the Aircraft design. Wind has great impact on the flight parameter. In order to accurately simulate the wind model and calculate the flight parameters  a simulation modeling method for flight parameter simulation platform under wind field environment is established. Firstly  the various sub-systems which affecting flight parameters are analyzed  some mathematical models of the flight parameter simulation platform is established. Secondly  the atmospheric wind field is studied to analyze the impact on its trajectory. Then the model is built in the Simulink toolbox in the Matlab which is based on the principles of hierarchy and modularity  using C MEX S-function for the complex kinetic equations. Finally  when the models have been established  encapsulating models for several subsystem and assembling them for the Aircraft simulation platform based on the unified interface. The simulation tests (including the performance test of a certain gliding Aircraft  the wind influence test of a certain uncontrolled aircraft) prove the simulation capability of the platform  and its calculating step can reach 1 ms. Comparing simulation with field test data of a certain uncontrolled aircraft  it shows that the relative deviation of range is 0.47%  the relative deviation of maximal altitude is 2.1%. Taking relevant standards as a reference standard  it is demonstrated the platform is reliable  meets the engineering accuracy requirements. 2010 IEEE.  


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