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Chinese Academy of Sciences Institutional Repositories Grid
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CAS IR Grid
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长春光学精密机械与物... [4]
力学研究所 [2]
海洋研究所 [2]
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OAI收割 [8]
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会议论文 [4]
期刊论文 [3]
CNKI期刊论文 [1]
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2022 [2]
2021 [1]
2020 [1]
2011 [2]
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A ratiometric fluorescent probe based on carbon dots assembly for intracellular lysosomal polarity imaging with wide range response
CNKI期刊论文
OAI收割
2022
作者:
Guangyue Zou
  |  
收藏
  |  
浏览/下载:1/0
  |  
提交时间:2024/12/18
Carbon dots
Polarity
Lysosome
Ratiometric sensing
Wide linear range
A ratiometric fluorescent probe based on carbon dots assembly for intracellular lysosomal polarity imaging with wide range response
期刊论文
OAI收割
CHINESE CHEMICAL LETTERS, 2022, 卷号: 33, 期号: 2, 页码: 778-782
作者:
Zou, Guangyue
;
Chen, Shuai
;
Liu, Nazhen
;
Yu, Yongliang
  |  
收藏
  |  
浏览/下载:87/0
  |  
提交时间:2022/04/12
Carbon dots
Polarity
Lysosome
Ratiometric sensing
Wide linear range
Wide linear range and highly sensitive flexible pressure sensor based on multistage sensing process for health monitoring and human-machine interfaces
期刊论文
OAI收割
CHEMICAL ENGINEERING JOURNAL, 2021, 卷号: 412, 页码: 10
作者:
Zhong Mengjuan
;
Zhang Lijuan
;
Liu Xu
;
Zhou Yaning
;
Zhang MY(张懋熠)
  |  
收藏
  |  
浏览/下载:41/0
  |  
提交时间:2021/05/17
Linear sensitivity
Wide range
Micro-patterns
Flexible pressure sensor
Human-machine interface
Exploiting ultra-large linear elasticity over a wide temperature range in nanocrystalline NiTi alloy
期刊论文
OAI收割
JOURNAL OF MATERIALS SCIENCE & TECHNOLOGY, 2020, 卷号: 57, 页码: 197-203
作者:
Sun Z
;
Hao SJ
;
Kang GF
;
Ren Y
;
Liu JP(刘俊鹏)
  |  
收藏
  |  
浏览/下载:34/0
  |  
提交时间:2020/11/30
NiTi
Nanocrystalline
Linear-elasticity
Wide temperature range
Twinning
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%
Control method research on wide flight envelope aerocraft (EI CONFERENCE)
会议论文
OAI收割
2nd Annual Conference on Electrical and Control Engineering, ICECE 2011, September 16, 2011 - September 18, 2011, Yichang, China
作者:
Duan Z.
收藏
  |  
浏览/下载:28/0
  |  
提交时间:2013/03/25
The flying qualities of aerocraft was directly effected by the autopilot
for the wide flight envelope aerocraft
on the basic of analyzing the typical trajectory
the three loop autopilots of roll stability
pitch and yaw were designed
using single-mode Transient suppression method
the overload due to control surface transition deflection was avoided when control parameters changing
the verification was done by non-linear simulation. The result showed that: Under the action of the disturbance torque
the maximum roll was less than 5
the range of the aerocraft was from 13.5km to 22.4km
the max height was about 5100m
the max deviation of lateral was about 42m
the maximum elevator deflection was less than 6.5 the control law was applicable within the effective range. An autopilot design method of wide flight envelope aerocraft was provided. 2011 IEEE.
Cr image enhancement based on human visual characteristics (EI CONFERENCE)
会议论文
OAI收割
2010 International Conference on Computer Design and Applications, ICCDA 2010, June 25, 2010 - June 27, 2010, Qinhuangdao, Hebei, China
Zhang M.-H.
;
Zhang Y.-Y.
收藏
  |  
浏览/下载:29/0
  |  
提交时间:2013/03/25
The characteristic of digital CR medicine radiation image has wide dynamic range
abundant details and bad contrast
so it is necessary to enhance CR image to the need of doctor diagnosis. But the general enhancement algorithms don't consider human visual characteristics
so it puts forward CR medicine image adaptive enhancement algorithm combining the human visual property
which is more sensitive to smooth area noise compared with detail area noise
and makes image edge detail enhancement great in detail area
and detail enhancement little in smooth area
in which factor K is based on space change of image domain
accordingly gaining non-linear enhancement edge details of CR image. Experiment results demonstrate that the algorithm enhances CR image detail and CR image enhanced has good visual effect
so the method is fit for edge detail enhancement of CR medicine radiation image. 2010 IEEE.
Design of a scene simulator in land-based aerospace lab with the man-made light source system based on quantum theory (EI CONFERENCE)
会议论文
OAI收割
Optoelectronic Devices and Integration II, November 12, 2007 - November 15, 2007, Beijing, China
作者:
Fang W.
;
Yi W.
收藏
  |  
浏览/下载:29/0
  |  
提交时间:2013/03/25
The paper presents a method with the technique of combination filtering of spectrum and the technique of DSP control for the simulation and recognition of the spontaneously lightening object and stellar map in the universe. The magnitude and the spectrum of a star can be simulated in a wide dynamic range. We established the mathematical models of the Vega's visible light spectrum and luminous flux density. Tungsten-halogen lamp as a light source is used to fit the linear light of the spontaneously lightening object in the universe. Through the experiment
it shows that the more sub-channels there are while filtering spectrum in the visible spectrum
and the more degrees the variable neutral density filters and the narrow-band attenuators have
more close to the actual spectrum the simulated spectrum is. It is proved that using the PID technique is beneficial to the output of the accurate and steady radiation from the light sources. The experiment shows that the using of this method can get perfect result in fitting and simulating the spectrum
magnitude and the stellar map of the spontaneously lightening object . The analysis of the consistent result and the experimental error is also discussed in detail in this paper.