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长春光学精密机械与... [15]
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专题:长春光学精密机械与物理研究所
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Simulation test system of CCD signal processor based on FPGA (EI CONFERENCE)
会议论文
2nd International Conference on Mechatronics and Applied Mechanics, ICMAM 2012, December 8, 2012 - December 9, 2012, Taiwan
Zhang D.
;
Liu D.-B.
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浏览/下载:27/0
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提交时间:2013/03/25
Simulation test system of CCD signal processor based on FPGA is proposed. Field-programmable gate array (FPGA) is applied as control processing core and used in the aerospace upgrade screening of industrial grade signal processor. The system functional composition and working principle were introduced in detail. Actually evaluation and testing system was completed with integrating the forty signal processor in a single board. The system has been successfully applied in the dynamic build-in screening test of industrial grade signal processor XRD98L63
the system work stably and reliability. Test result is zero on the nonconforming product rate
satisfying the qualification that single batch screening nonconforming rate is less than 5%
build-in screening of industrial grade components for the space load applications is implemented. (2013) Trans Tech Publications
Switzerland.
Research on the torque characteristic of disc micromotor on axial magnetic field (EI CONFERENCE)
会议论文
2012 2nd International Conference on Consumer Electronics, Communications and Networks, CECNet 2012, April 21, 2012 - April 23, 2012, Three Gorges, China
Liu B.
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浏览/下载:46/0
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提交时间:2013/03/25
In order to increase the electromagnetic torque density of micromotor with axial magnetic field
numerical analysis of permanent magnetic field and electromagnetic torque were deduced and the key factors of increasing torque density of micromotor was obtained. The numerical analysis of three-dimensional magnetic field in air gap produced by spliced sector permanent magnetic poles is done
and the way of improving flux density and permanent magnet use efficiency are given through investigating the influence of magnet thickness
height of air gap and pole interval rate and other parameters to air gap flux density and leakage flux. Based on the test of axial magnetic field and torque characteristic of micromotor
the analysis of micromotor magnetic field and calculation of torque are verified
meanwhile using the plane stator with 0.7mm thickness assemble micromotor having minimum air gap height of 1mm and its torque constant up to 3.8mNm/A. 2012 IEEE.
Study of horizontal shafting with spherical four-way structure (EI CONFERENCE)
会议论文
2012 International Conference on Optoelectronics and Microelectronics, ICOM 2012, August 23, 2012 - August 25, 2012, Changchun, China
Yang L.
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浏览/下载:17/0
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提交时间:2013/03/25
Altazimuth photoelectric theodolite level shaft U-type and T-type structure
but with the expanding field of applications of photoelectric theodolite
the horizontal shaft structure occur great changes. For example
in the marine environment
shipboard conditions
the instrument has a waterproof
corrosion-resistant
easy maintenance and other functions
while carrier-based optoelectronic devices from a single visible television configure the development of integrated infrared system and ranging system as one of the single-station measurement system
due to the spherical structure has sufficient internal space exactly adapted to this need. In this paper
the horizontal axis of a spherical four-way structure. From aspects of the spherical four-way split in the form and shafting design and finite element analysis of the detailed design. A spherical four-way horizontal axis system
diameter 550mm
weight 19kg sphere
in the 40kg load
the maximum deformation of 3.3m
fully meet the requirements. The shaft of the structure of the shaking is less than 2 arc seconds
the vibration test
the re-examination instrument accuracy change is less than 1 arc seconds. Verify that the structure is stable and reliable. 2012 IEEE.
Efficient rate control technique for CCSDS image encoding (EI CONFERENCE)
会议论文
IEEE 2nd International Conference on Computing, Control and Industrial Engineering, CCIE 2011, August 20, 2011 - August 21, 2011, Wuhan, China
Jin L.
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浏览/下载:85/0
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提交时间:2013/03/25
For the limitation of data transmission bandwidth and real time transmission demand
generally image compression is required to implement the precise and flexible rate control algorithm. Rate control is an important issue in the image compression field. This paper considers the problem of rate allocation to each encoded segment for CCSDS image compression. One straightforward method is to allocate an equal amount of rate to each segment based on the average of the total number of compressed bytes. The obvious drawback of this method is that different segment will be reconstructed to different quality
so the overall quality of the reconstructed image will not be optimized. For the shortage of the original rate control method
as to improve the overall quality of the reconstructed image
an improved rate control algorithm is proposed for CCSDS image encoding. The key component of the proposed rate control method is the appropriate rate allocation. Experiments on the test images show that the PSNR can be increased at about 0.3dB on average
compared to the original algorithm. Therefore
experimental results confirm the effectiveness of the proposed algorithm in terms of objective evaluation
and the rate-distortion performance of the reconstructed image is improved. 2011 IEEE.
Double inverted pendulum control based on three-loop PID and improved BP neural network (EI CONFERENCE)
会议论文
2011 2nd International Conference on Digital Manufacturing and Automation, ICDMA 2011, August 5, 2011 - August 7, 2011, Zhangjiajie, Hunan, China
Sang Y.
;
Fan Y.
;
Liu B.
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浏览/下载:28/0
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提交时间:2013/03/25
To deal with the defects of BP neural networks used in balance control of inverted pendulum
such as longer train time and converging in partial minimum
this article reaLizes the control of double inverted pendulum with improved BP algorithm of artificial neural networks(ANN)
builds up a training model of test simulation and the BP network is 6-10-1 structure. Tansig function is used in hidden layer and PureLin function is used in output layer
LM is used in training algorithm. The training data is acquried by three-loop PID algorithm. The model is learned and trained with Matlab calculating software
and the simuLink simulation experiment results prove that improved BP algorithm for inverted pendulum control has higher precision
better astringency and lower calculation. This algorithm has wide appLication on nonLinear control and robust control field in particular. 2011 IEEE.
Buffer and vibration optimization of missile data recorder structure (EI CONFERENCE)
会议论文
2011 International Conference on Mechatronics and Materials Processing, ICMMP 2011, November 18, 2011 - November 20, 2011, Guangzhou, China
Zhang J.
;
Jia H. G.
;
Ding L.
;
Dong W. H.
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浏览/下载:19/0
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提交时间:2013/03/25
On the analysis of the original data recorder
the stress wave theory is the elastic theory can explain the filter buffer question from the micro-small space
made several key problems clear when buffer and damping
from this designed a composite structure for vibration reduction
distinguished between a cushion theory and application field of stress wave theory
which made the dynamic stress of protected component down about one order of magnitude. Optimization with Isight and Ls-dyna
the traditional rigid spring-buffer model whose object is to reduce the impact of acceleration that can not accurately describe the elastic force of the part of the actual situation
the protected component's dynamic stress down about 69.3% and the data recorder's quality 300g lower
finally passed the Marshall Hammer test successfully. 2011 Trans Tech Publications.
DVI interface, optical fiber video transceiver used in LED display system (EI CONFERENCE)
会议论文
2011 IEEE 3rd International Conference on Communication Software and Networks, ICCSN 2011, May 27, 2011 - May 29, 2011, Xi'an, China
Li S.
;
Wang R.
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浏览/下载:17/0
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提交时间:2013/03/25
A professional DVI-Video optical fiber transceiver was designed based on FPGA (Field Programmable Gate Array) in order to meet the need of real-time LED display. The system could be used to transmit a non-loss
real-time video source whose resolution was 1024 768 and refresh rate was 60Hz in a single mode optical fiber. The top-down design method was used while programming FPGA. Some module design ideas were discussed including video data acquisition
caching
framing
frame detecting and video reproducing. The required bandwidth of each module was analyzed and calculated in details. Some relevant simulation results were also given. In practical test
real-time video display was achieved. And the transmission rate of coded data was up to 2Gbps
and the transmission distance could reach 10km. 2011 IEEE.
System design on a field emission with phosphor detection (EI CONFERENCE)
会议论文
2009 International Symposium on Liquid Crystal Science and Technology, August 2, 2009 - August 5, 2009, Kunming, China
An J.
;
Deng C.
;
Li Y.
;
Sun T.
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浏览/下载:14/0
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提交时间:2013/03/25
It is well-known that the phosphor is widely used for the field emission display (FED)
and its luminescent and temperature properties are very important for the effect of display. In this paper
we propose a measurement scheme for the phosphor
and design a test-equipment to test the luminescent and temperature properties of phosphor. Furthermore
the equipment can also be used for the life-test of the phosphor because it can generate a great excitation power. Finally
there are design principle
structure and some data and result which we obtained in the experiment. These data will be very useful for the design of FED. (2010) Trans Tech Publications.
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.
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浏览/下载:23/0
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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.
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浏览/下载:19/0
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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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