中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
首页
机构
成果
学者
登录
注册
登陆
×
验证码:
换一张
忘记密码?
记住我
×
校外用户登录
CAS IR Grid
机构
长春光学精密机械与物... [3]
自动化研究所 [1]
沈阳自动化研究所 [1]
采集方式
OAI收割 [5]
内容类型
会议论文 [4]
学位论文 [1]
发表日期
2019 [1]
2012 [1]
2010 [1]
2009 [1]
2005 [1]
学科主题
筛选
浏览/检索结果:
共5条,第1-5条
帮助
条数/页:
5
10
15
20
25
30
35
40
45
50
55
60
65
70
75
80
85
90
95
100
排序方式:
请选择
题名升序
题名降序
提交时间升序
提交时间降序
作者升序
作者降序
发表日期升序
发表日期降序
Design and Experiment of Deep-sea Energy-storage Buoyancy Regulating System
会议论文
OAI收割
Marseille, France, June 17-20, 2019
作者:
Bai YF(白云飞)
;
Zhang QF(张奇峰)
;
Zhang AQ(张艾群)
;
Li S(李硕)
;
Chen, Jjn
  |  
收藏
  |  
浏览/下载:31/0
  |  
提交时间:2019/12/23
buoyancy regulating
low-energy consumption
experimental prototype
pressure experiment
Design of a miniature axial flux flywheel motor with PCB winding for nanosatellites (EI CONFERENCE)
会议论文
OAI收割
2012 International Conference on Optoelectronics and Microelectronics, ICOM 2012, August 23, 2012 - August 25, 2012, Changchun, China
Wu J.
收藏
  |  
浏览/下载:39/0
  |  
提交时间:2013/03/25
This paper presents the design and analysis of an axial flux permanent-magnet (AFPM) machine for nanosatellites application. It is a miniature axial flux surface mounted permanent magnet flywheel motor
using a printed circuit board (PCB) stator winding. The PCB stator has simplified the design and construction and avoids unnecessary space
since size reduction has become one of the most important aspects of flywheel motor design for nanosatellites. The performances of the machine are estimated by combination method of three-dimensional (3D) electromagnetic finite element analysis (FEA) and approximate theoretical analysis. The back EMF and electromagnetic torque are derived. A comparison between the analysis and experimental measurement results of the prototype machine is also presented. Both simulated and experimental results show that the proposed motor would be an acceptable solution for the nanosatellite applications with advantages such as simple structure and low-cost
as multi-layer circuit board production techniques have made the production of printed circuit coils cheaper and easier. 2012 IEEE.
In situ long trace profiler for measurement of Wolter type-I mirror (EI CONFERENCE)
会议论文
OAI收割
Advances in Metrology for X-Ray and EUV Optics III, August 1, 2010 - August 2, 2010, San Diego, CA, United states
作者:
Chen B.
;
Chen B.
收藏
  |  
浏览/下载:27/0
  |  
提交时间:2013/03/25
The surface profile of Wolter type-I mirror has a great impact on the performance of Solar X-ray Telescope. According to the existing fabrication instrument and experimental conditions in our lab
an in situ Long Trace Profiler is developed and set up on the fabrication instrument in order to measure the surface profile of Wolter mirror in real time during fabrication process. Its working mechanism
structural parameters and data processing algorithm are investigated. The prototype calibrated by a standard plane mirror is used to measure a sample of Wolter type-I mirror. The results show that our prototype can achieve an accuracy of 2.6rad rms for slope error with a stability of 1.33rad during the whole measurement period. This can meet further fabrication requirements. 2010 Copyright SPIE - The International Society for Optical Engineering.
面向智能空间的位置感知计算研究
学位论文
OAI收割
工学博士, 中国科学院自动化研究所: 中国科学院研究生院, 2009
作者:
姚庆明
收藏
  |  
浏览/下载:64/0
  |  
提交时间:2015/09/02
智能空间
位置感知计算
原型实验系统
信号特性
传感器模型
状态空间模型
动态贝叶斯网络
Intelligent Space
Location-Aware Computing
Experimental Prototype
Signal Characteristics
Sensor Models
State Space Model
Dynamic Bayesian Network
CMOS APS imaging system application in star tracker (EI CONFERENCE)
会议论文
OAI收割
Advanced Materials and Devices for Sensing and Imaging II, November 8, 2004 - November 10, 2004, Beijing, China
作者:
Li J.
;
Liu Y.
;
Liu Y.
;
Liu Y.
;
Liu J.
收藏
  |  
浏览/下载:56/0
  |  
提交时间:2013/03/25
Small satellites are capable of performing space explore missions that require accurate attitude determination and control. However
low weight
size
power and cost requirements limit the types of attitude sensor of small craft
such as CCD
are not practical for small satellites. CMOS APS is a good substitute for attitude sensors of small craft. Some of the technical advantages of CMOS APS are no blooming
single power
low power consumption
small size and little support circuitry
direct digital output
simple to system design
in particular
radiation-hard characteristic compare with CCD. This paper discusses the application probability of CMOS APS in star tracker for small satellites
further more
a prototype ground-based star camera based on STAR250 CMOS image sensor has been built. In order to extract stars positions coordinates
subpixel accuracy centroiding algorithm has been developed and tested on some ground-based images. Moreover
the camera system star sensitivity and noise model are analyzed
and the system accuracy is been evaluated. Experimental results indicate that a star camera based on CMOS APS is a viable practical attitude sensor appropriate for space small satellites.