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长春光学精密机械与... [25]
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A Universal Size Design Principle for Stretchable Inorganic Electronics to Work Consistently under Different Interface Conditions
期刊论文
OAI收割
ADVANCED FUNCTIONAL MATERIALS, 2022, 页码: 9
作者:
Li, Shuang
;
Lan, Yuqun
;
Huang, YongAn
;
Chen, Yuli
;
Su, Yewang
  |  
收藏
  |  
浏览/下载:16/0
  |  
提交时间:2023/02/09
consistency
design principle
interface conditions
stretchable inorganic electronics
Robust error based non-collocated output tracking control for a heat equation
期刊论文
OAI收割
AUTOMATICA, 2020, 卷号: 114, 页码: 11
作者:
Guo, Bao-Zhu
;
Meng, Tingting
  |  
收藏
  |  
浏览/下载:25/0
  |  
提交时间:2020/05/24
Internal model principle
Observer design
Output tracking
Disturbance rejection
Longitudinal control law design and simulation of fixed-wing UAV (EI CONFERENCE)
会议论文
OAI收割
2012 International Conference on Measurement, Instrumentation and Automation, ICMIA 2012, September 15, 2012 - September 16, 2012, Guangzhou, China
作者:
Duan Z.
收藏
  |  
浏览/下载:27/0
  |  
提交时间:2013/03/25
Taken some fixed-wing UAV as the study object
the aircraft movement was broken down into the longitudinal movement and lateral movement according to the linearized small perturbation principle
the longitudinal control law design method was discussed using root locus which belonged to classical control theory. The six degrees of freedom nonlinear model simulation result shows that: the control parameters designed are reasonable
the simulation profile is fully consistent with the setting profile
the control effect of pitch angle loop and altitude loop meets with the indices requirements
the method is mature and reliable
easy to realize in engineering. (2013) Trans Tech Publications
Switzerland.
Parameter optimization of passive dynamic walking biped with knees (EI CONFERENCE)
会议论文
OAI收割
2012 2nd International Conference on Materials Science and Information Technology, MSIT 2012, August 24, 2012 - August 26, 2012, Xi'an, Shaan, China
作者:
Zhang P.
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2013/03/25
A method to find the optimized parameter values of passive dynamic walking biped is presented. The effects of biped physical parameters on the stability property of passive gaits are studied by simulation experiments. The chosen parameters include the mass distribution
length of leg and slope angle. The stability property of passive walking limit cycles is used as criterion of optimization calculation
including the orbital stability described by eigen-values of linearized Poincare map and the global property described by size of attraction region. The simulation results show how the stability of limit cycle varies when physical parameters of the passive biped change. The work is useful to explore the inherent property of passive dynamic walking and can be used as an important instruction in the mechanical design of biped robots based on principle of passive dynamic walking. (2012) Trans Tech Publications
Switzerland.
The analyze and design of focusing system for space camera (EI CONFERENCE)
会议论文
OAI收割
2012 International Conference on Electrical Insulating Materials and Electrical Engineering, EIMEE 2012, May 25, 2012 - May 27, 2012, Shenyang, Liaoning, China
作者:
Yu T.
收藏
  |  
浏览/下载:27/0
  |  
提交时间:2013/03/25
In order to control the focal plane and guarantee the imaging quality of space camera
the focusing system was proposed. Firstly
the reasons of defocusing were analyzed and a solution method was given. Secondly
the system structure and operating principle were introduced. Thirdly
the system design was presented in detail. Finally
the system was experimented. Experimental results indicate that the defocusing amount of camera can be controlled below 10 um and the focusing system satisfies the requirement of system design. (2012) Trans Tech Publications
Switzerland.
Three-loop autopilot design and simulation (EI CONFERENCE)
会议论文
OAI收割
2012 9th IEEE International Conference on Mechatronics and Automation, ICMA 2012, August 5, 2012 - August 8, 2012, Chengdu, China
作者:
Zhang Y.
收藏
  |  
浏览/下载:44/0
  |  
提交时间:2013/03/25
In order to realize missile real-time change flight trajectory
three-loop autopilot is setting up. The structure characteristics
autopilot model
and control parameters design method were researched. Firstly
this paper introduced the 11th order three-loop autopilot model. With the principle of systems reduce model order
the 5th order model was deduced. On that basis
open-loop frequency characteristic and closed-loop frequency characteristic were analyzed. The variables of velocity ratio
dynamic pressure ratio and elevator efficiency ratio were leading to correct system nonlinear. And then autopilot gains design method were induced. System flight simulations were done
and result shows that autopilot gains played a good job in the flight trajectory
autopilot satisfied the flight index. 2012 IEEE.
The design of computer-generated holograms for testing unsymmetrical optical surfaces (EI CONFERENCE)
会议论文
OAI收割
2012 International Symposium on Photonics and Optoelectronics, SOPO 2012, May 21, 2012 - May 23, 2012, Shanghai, China
作者:
Zhang X.
;
Zhang Y.
;
Zhang X.
;
Zhang X.
收藏
  |  
浏览/下载:27/0
  |  
提交时间:2013/03/25
It is a technical difficulty to test the unsymmtrical optical surfaces in non-contact methods. But we can do it using computer-generated holograms (CGH). The principle and design of the CGH have been discussed in the paper. Take the cubic suface as an example
The order separation of the CGH is analyzed theoretically and the simulation result of the order separation is given in the paper. We develop the binary process of the continuous CGH phase function and get the sample of the amplitude CGH. A CGH for testing a cubic phase plate with duty cycle 0.5 is fabricated by using e-beam lithographic techniques. In this situation
the contrast of the interference fringe pattern can achieve a level of 99.4% by calculation. 2012 IEEE.
Laser pulse coded signal frequency measuring device based on DSP and CPLD (EI CONFERENCE)
会议论文
OAI收割
International Symposium on Photoelectronic Detection and Imaging 2011: Laser Sensing and Imaging; and Biological and Medical Applications of Photonics Sensing and Imaging, May 24, 2011 - May 26, 2011, Beijing, China
作者:
Zhang H.-B.
;
Wang T.-F.
;
Guo R.-H.
;
Li Y.
;
Li Y.
收藏
  |  
浏览/下载:38/0
  |  
提交时间:2013/03/25
Laser pulse code is an anti-jamming measures used in semi-active laser guided weapons. On account of the laser-guided signals adopting pulse coding mode and the weak signal processing
it need complex calculations in the frequency measurement process according to the laser pulse code signal time correlation to meet the request in optoelectronic countermeasures in semi-active laser guided weapons. To ensure accurately completing frequency measurement in a short time
it needed to carry out self-related process with the pulse arrival time series composed of pulse arrival time
calculate the signal repetition period
and then identify the letter type to achieve signal decoding from determining the time value
number and rank number in a signal cycle by Using CPLD and DSP for signal processing chip
designing a laser-guided signal frequency measurement in the pulse frequency measurement device
improving the signal processing capability through the appropriate software algorithms. In this article
we introduced the principle of frequency measurement of the device
described the hardware components of the device
the system works and software
analyzed the impact of some system factors on the accuracy of the measurement. The experimental results indicated that this system improve the accuracy of the measurement under the premise of volume
real-time
anti-interference
low power of the laser pulse frequency measuring device. The practicality of the design
reliability has been demonstrated from the experimental point of view.
SGCMG design and time accumulation error analysis (EI CONFERENCE)
会议论文
OAI收割
2011 International Conference on Mechatronic Science, Electric Engineering and Computer, MEC 2011, August 19, 2011 - August 22, 2011, Jilin, China
Xu W.
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2013/03/25
SGCMG receives much concern due to the performance of its excellent torque output on spacecraft control
it has been applied to large foreign spacecraft already
but late start and only limited to configurations and steering law study in China. Based on the needs of agility small satellites
this article explained the method of SGCMG principle prototype design and proposed the influence on SGCMG output torque precision generated by time accumulation error first time. This article provided a new idea for future SGCMG project development and had good reference value for SGCMG research. 2011 IEEE.
Design of thermostat system based on Proteus simulation software (EI CONFERENCE)
会议论文
OAI收割
2011 International Conference on Electronic and Mechanical Engineering and Information Technology, EMEIT 2011, August 12, 2011 - August 14, 2011, Harbin, China
Han Z.
;
Song K.
收藏
  |  
浏览/下载:39/0
  |  
提交时间:2013/03/25
In order to solve the problem of precise temperature control
the thermoelectric cooler (TEC) principle widely used is analyzed for the design of the whole control process and selection of control parameters
and then accurate simulation model of the TEC is established in Proteus simulation software. Moreover
combined with the traditional circuit simulation model
the temperature control loop is designed
and the response characteristics of the system are tested using an input signal similar to the unit-step function to achieve the precise temperature control. Simulation results show that the proposed control circuits can precisely convert error signal to output voltage sent to TEC model
and TEC model behaves approximately like a two-pole system. The first pole starts at 20mHz and a second pole at 1Hz. 2011 IEEE.