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机构
长春光学精密机械与物... [3]
西安光学精密机械研究... [2]
深海科学与工程研究所 [1]
采集方式
OAI收割 [6]
内容类型
会议论文 [4]
期刊论文 [2]
发表日期
2022 [2]
2020 [1]
2011 [2]
2007 [1]
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A Tracking Imaging Control Method for Dual-FSM 3D GISC LiDAR
期刊论文
OAI收割
Remote Sensing, 2022, 卷号: 14, 期号: 13
作者:
Cao, Yu
;
Su, Xiuqin
;
Qian, Xueming
;
Wang, Haitao
;
Hao, Wei
  |  
收藏
  |  
浏览/下载:55/0
  |  
提交时间:2022/08/25
3D GISC LiDAR
dual-FSM tracking and aiming
FSM feedback decoupling
composite axis control
remote-sensing imaging
Research on Key Technology of Compound Axis Control of Periscope Optical Communication Terminal
会议论文
OAI收割
Chongqing, China, 2022-03-04
作者:
Liu, Peng
;
Li, Zhiguo
;
Xie, Meilin
;
Wang, Fan
;
Liu, Bo
  |  
收藏
  |  
浏览/下载:139/0
  |  
提交时间:2022/04/27
Composite axis control system
Bandwidth matching
Image rotation
A New Composite Spiral Scanning Approach for Beaconless Spatial Acquisition and Experimental Investigation of Robust Tracking Control for Laser Communication System with Disturbance
期刊论文
OAI收割
IEEE PHOTONICS JOURNAL, 2020, 卷号: 12, 期号: 6, 页码: 13
作者:
Zhang, Min
;
Li, Bo
;
Tong, Shoufeng
  |  
收藏
  |  
浏览/下载:32/0
  |  
提交时间:2021/03/23
Spirals
Laser beams
Target tracking
Uncertainty
Heuristic algorithms
Actuators
Laser modes
Optical communication
beaconless spatial acquisition
composite spiral scanning
dynamic tracking assembly
multiple-axis control
Design and test of pointing mirror assembly for spaceborne remote sensing camera (EI CONFERENCE)
会议论文
OAI收割
2011 International Conference on Electronics, Communications and Control, ICECC 2011, September 9, 2011 - September 11, 2011, Ningbo, China
作者:
Chen W.
收藏
  |  
浏览/下载:34/0
  |  
提交时间:2013/03/25
In order to ensure the surface figure of the pointing mirror (460mm long
290mm wide) in spaceborne remote sensing camera
Silicon Carbide was selected as the mirror material. The form of composite triangular and rectangular and the combination of open and closed back was explored in the lightweight design. A new kinematic mount and flexible structure in axis is used to hold the mirror around the lateral surface. The structure can minimize distortions induced by coefficient of thermal expansion mismatch among the materials. This eliminates the bending of the integral mount under the weight of the mirror. Optical performance of the mirror was analyzed under gravity load and temperature load using finite element method. Predicted surface figure error based on the removal of bias
tilt and power was calculated using an in-house Matlab script for mirrors. The pointing mirror assembly was tested using open loop servo control. And the surface figure was checked using interferometer. Surface figure accuracy is better than 1/30 ( 632.8nm
rms). The results show that the kinematic mount induces minimal figure error on the optical surface. 2011 IEEE.
Application of particulate reinforced aluminum matrix composite in airborne photoelectric turret (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
作者:
Wang P.
收藏
  |  
浏览/下载:24/0
  |  
提交时间:2013/03/25
In order to design and manufacture more excellent airborne photoelectric stable turret
modulus of elasticity of 213 GPa and thermal expansion coefficient of 7.9106/K. The frame has decreased the maximum deformation by by 60% and increased the fundamental frequency by 65% as compared with those of aluminum alloy materials
a new type of aeronautical material-particulate reinforced aluminum matrix composite (SiC/Al composite) is investigated. Several crucial technologies
respectively as shown by finite element analysis results. Those are confirmed by vibration test furthermore. Therefore
such as pressureless infiltration technology
a significant lightening effect is achieved and the thermal control load is also reduced. The test result indicates that the stable accuracy of the system achieves 19.8rad and the optical-axis parallelism of pay load is 0.1mrad. The research applies the SiC/Al composites to airborne photoelectric platforms
interface reaction controls and plate's welding are systematically studied. Then
which makes a effective exploration for the new aeronautical material's application. 2011 IEEE.
using SiC/Al composites
the airborne photoelectric stable turret frame is successfully prepared in density of 2.94 g/ cm3
Research on shaftless fast-steering mirror used in a precision tracking-aiming system (EI CONFERENCE)
会议论文
OAI收割
3rd International Symposium on Advanced Optical Manufacturing and Testing Technologies, AOMATT 2007: Large Mirrors and Telescopes, July 8, 2007 - July 12, 2007, Chengdu, China
作者:
Wang Y.
;
Guo J.
;
Guo J.
;
Wang Y.
;
Wang Y.
收藏
  |  
浏览/下载:25/0
  |  
提交时间:2013/03/25
Based on the analysis of principle of tracking and aiming system
some important factors to design the structure of tracking-aiming system and the layout of optical system are discussed. Besides
the paper gives the present developing situation of fast-steering mirror at home and abroad
analyzes the advantages and disadvantages of FSM with axis
and presents a novel design of flexible axis FSM. The main axis of composite axis system is tracked by motor to drive the frame
and the sub-axis is tracked by voice coil motor (VCM) to drive FSM. The structure of FSM and designing principle of VCM are introduced
and the emulation analyses of inherent frequency and deformation under load of the FSM with software COSMOS are also given.