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Chinese Academy of Sciences Institutional Repositories Grid
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CAS IR Grid
机构
国家空间科学中心 [1]
数学与系统科学研究院 [1]
云南天文台 [1]
国家授时中心 [1]
采集方式
OAI收割 [4]
内容类型
期刊论文 [3]
会议论文 [1]
发表日期
2022 [3]
2012 [1]
学科主题
电子、通信与自动控制... [1]
空间技术 [1]
计算机科学技术 [1]
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A Multi-Target Passive Location Method Based on GDOP Value and Beam Resolution
期刊论文
OAI收割
INTERNATIONAL JOURNAL OF PATTERN RECOGNITION AND ARTIFICIAL INTELLIGENCE, 2022, 卷号: 36, 期号: 8
作者:
Miao, Sheng
;
Dong, Liang
;
Wang, Xiaorui
  |  
收藏
  |  
浏览/下载:40/0
  |  
提交时间:2022/07/18
Sensor network
time difference of arrival
multi-target location
unsupervised clustering
narrow-band beam forming
Localizability With Range-Difference Measurements: Numerical Computation and Error Bound Analysis
期刊论文
OAI收割
IEEE-ACM TRANSACTIONS ON NETWORKING, 2022, 页码: 14
作者:
Zeng, Guangyang
;
Mu, Biqiang
;
Wei, Jieqiang
;
Wong, Wing Shing
;
Wu, Junfeng
  |  
收藏
  |  
浏览/下载:43/0
  |  
提交时间:2022/06/21
Location awareness
Noise measurement
Error analysis
Pollution measurement
Measurement uncertainty
Coordinate measuring machines
Closed-form solutions
Localization
time difference of arrival (TDOA)
nonconvex optimization
numerical computation
Lagrange multiplier
基于时差频差的双星无源定位地基差分技术研究
期刊论文
OAI收割
时间频率学报, 2022, 卷号: 45, 期号: 4, 页码: 294
作者:
薛艳荣
;
肖波
;
李雨薇
;
刘娅
;
李孝辉
  |  
收藏
  |  
浏览/下载:14/0
  |  
提交时间:2023/12/13
dual-satellite passive positioning
time difference of arrival
frequency difference of arrival
positioning accuracy
双星无源定位
到达时间差
到达频率差
定位精度
AUTONOMOUS INTEGRATED NAVIGATION USING X-RAY PULSARS AND ASTEROIDS
会议论文
OAI收割
63rd International Astronautical Congress 2012, IAC 2012, Naples, Italy, 2012
Yang Chengwei
;
Gao Dong
;
Zheng Jianhua
收藏
  |  
浏览/下载:38/0
  |  
提交时间:2014/04/30
To improve the navigation performance of the spacecraft during interplanetary cruise
a novel integrated navigation system is proposed. For X-ray pulsar navigation (XNAV) is a hot and prospective research subject
and the optical navigation using asteroids is practical in space engineering
we designed an autonomous navigation system using one X-ray detector and one navigation camera. The measurement models of the XNAV based on the time difference of arrival and the optical navigation based on the images of asteroids are presented. To enhance practicality
the X-ray pulsars and asteroids are observed by turns. The batch least square filter
used by Deep Space I
is adopted to estimate the system state. The numerical simulation results show that the integrated navigation is feasible on the interplanetary cruise orbit. Moreover
compared with the XNAV and the optical navigation
the integrated navigation system can provide higher navigation performance.