机构

• 上海天文台 [4]
• 国家天文台 [3]
• 地质与地球物理研究所 [1]
• 长春光学精密机械与物... [1]
• 国家授时中心 [1]

采集方式

• OAI收割 [10]

内容类型

• 期刊论文 [9]
• 会议论文 [1]

发表日期

• 2023 [1]
• 2016 [1]
• 2015 [2]
• 2013 [1]
• 2012 [3]
• 2010 [2]
• 更多

学科主题

筛选

浏览/检索结果: 共10条，第1-10条 帮助 条数/页： 5101520253035404550556065707580859095100 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 Prediction of geosynchronous electron fluxes using an artificial neural network driven by solar wind parameters 期刊论文  OAI收割 ADVANCES IN SPACE RESEARCH, 2023, 卷号: 71, 期号: 1, 页码: 275-285 作者:  Wang, Jianhang;  Guo, Deyu;  Xiang, Zheng;  Ni, Binbin;  Liu, Yangxizi   |  收藏  |  浏览/下载：27/0  |  提交时间：2023/03/30 Flux prediction  Artificial neural network  Geosynchronous orbit  Solar wind parameters   Applications of two-way satellite time and frequency transfer in the BeiDou navigation satellite system 期刊论文  OAI收割 SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 10 作者:  Zhou ShanShi;  Hu XiaoGong;  Liu Li;  Guo Rui;  Zhu LingFeng   |  收藏  |  浏览/下载：18/0  |  提交时间：2021/12/06 ORBIT  BDS  TWSTFT  satellite clock  prediction accuracy  system reference time  Allan variance   Orbit improvement for Chang'E-5T lunar returning probe with GNSS technique 期刊论文  OAI收割 ADVANCES IN SPACE RESEARCH, 2015, 卷号: 56, 期号: 11, 页码: 2473-2482 作者:  Fan, Min;  Hu, XiaoGong;  Dong, Guangliang;  Huang, Yong;  Cao, Jianfeng 收藏  |  浏览/下载：70/0  |  提交时间：2016/01/14 Chinese lunar exploration program  Global navigation satellite system  Weak signal acquisition and tracking performance  Fusion processing of space- and ground-based data  Accuracy of orbit determination and prediction   Long-term orbit prediction for Tiangong-1 spacecraft using the mean atmosphere model 期刊论文  OAI收割 ADVANCES IN SPACE RESEARCH, 2015, 卷号: 55, 期号: 5, 页码: 1432-1444 作者:  Tang, Jingshi;  Liu, Lin;  Cheng, Haowen;  Hu, Songjie;  Duan, Jianfeng 收藏  |  浏览/下载：38/0  |  提交时间：2016/12/01 Tiangong-1 spacecraft  Long-term orbit prediction  Mean atmosphere model   Satellite orbit determination combining C-band ranging and differenced ranges by transfer 期刊论文  OAI收割 CHINESE SCIENCE BULLETIN, 2013, 卷号: 58, 期号: 19, 页码: 2323-2328 作者:  Yang Ying;  Yang XuHai;  Li ZhiGang;  Feng ChuGang 收藏  |  浏览/下载：23/0  |  提交时间：2015/08/03 differenced ranges by transfer  orbital overlapping  orbit prediction   Satellite orbit determination by transfer with differenced ranges 期刊论文  OAI收割 CHINESE SCIENCE BULLETIN, 2012, 卷号: 57, 期号: 36, 页码: 4701-4706 作者:  Yang Ying;  Li ZhiGang;  Yang XuHai;  Feng ChuGang;  Cao Fen 收藏  |  浏览/下载：36/0  |  提交时间：2015/08/04 transfer  differenced ranges  precise orbit determination (POD)  orbit prediction   Satellite orbit determination by transfer with differenced ranges 期刊论文  OAI收割 CHINESE SCIENCE BULLETIN, 2012, 卷号: 57, 期号: 36, 页码: 4701 作者:  Yang Ying;  Li ZhiGang;  Yang XuHai;  Feng ChuGang;  Cao Fen   |  收藏  |  浏览/下载：18/0  |  提交时间：2021/11/29 GEOSTATIONARY SATELLITES  transfer  differenced ranges  precise orbit determination (POD)  orbit prediction   Satellite orbit determination by transfer with differenced ranges 期刊论文  OAI收割 CHINESE SCIENCE BULLETIN, 2012, 卷号: 57, 期号: 36, 页码: 4701 作者:  Yang Ying;  Li ZhiGang;  Yang XuHai;  Feng ChuGang;  Cao Fen   |  收藏  |  浏览/下载：17/0  |  提交时间：2021/12/06 GEOSTATIONARY SATELLITES  transfer  differenced ranges  precise orbit determination (POD)  orbit prediction   Orbit determination and prediction accuracy analysis for a regional tracking network 期刊论文  OAI收割 SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2010, 卷号: 53, 期号: 6, 页码: 1130-1138 作者:  Zhou ShanShi;  Hu XiaoGong;  Wu Bin 收藏  |  浏览/下载：23/0  |  提交时间：2015/08/19 orbit determination and prediction  regional tracking network  URE   Research of error correction of LEO satellite orbit prediction for vehicle-borne tracking and position device (EI CONFERENCE) 会议论文  OAI收割 2010 International Conference on Computer, Mechatronics, Control and Electronic Engineering, CMCE 2010, August 24, 2010 - August 26, 2010, Changchun, China 作者:  Wang J.-J.;  Guo L.-H. 收藏  |  浏览/下载：27/0  |  提交时间：2013/03/25 Vehicle-borne tracking and position device is used to track LEO satellite. Because of the absence of the target which might be caused by cloud or zenith blind zone  the forecasting data will be used to acquire the target. While orbit prediction has serious errors  the target is always missed. Meanwhile  in its application to the vehicle-borne tracking and position device  due to the base of instability in the tracking process  it will result in significant difference between predicting data and tracking data  so the target will be not tracked rapidly. We applied tracking data to predict satellite orbits by improving Laplace method  and then corrected the error between Predicted data and actual measured data by interpolation method of Lagrange which improves the accuracy of prediction values. The testing data shows the accuracy of predicted data ranging from 3' to 10" for both azimuth and elevation when extrapolated satellite orbit to 7 seconds time. 2010 IEEE.