国家自然科学基金(11073047)

作品数:12被引量:140H指数:7
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相关作者:黄勇宋叶志胡小工李培佳罗恒光更多>>
相关机构:中国科学院上海天文台北京航天飞行控制中心中国科学院大学中国电子科技集团第五十四研究所更多>>
相关期刊:《飞行器测控学报》《Science China(Physics,Mechanics & Astronomy)》《Science Bulletin》《航天器工程》更多>>
相关主题:VLBIUSINGGEOCARRIERSATELLITES更多>>
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Spacecraft Doppler tracking with possible violations of LLI and LPI:upper bounds from one-way measurements on MEX
《Research in Astronomy and Astrophysics》2015年第10期1751-1757,共7页Yi Xie Yong Huang 
funded by the National Natural Science Foundation of China(Grant Nos.11103010,11573015 and 11073047);the Fundamental Research Program of Jiangsu Province of China under No.BK2011553;the Research Fund for the Doctoral Program of Higher Education of China(No.20110091120003);the Fundamental Research Funds for the Central Universities(Grant No.20620140586);the Opening Project of Shanghai Key Laboratory of Space Navigation and Position Techniques(Grant No.14DZ2276100)
We analyze the post-fit residuals of one-way Doppler tracking data from the Mars Express (MEX) spacecraft to test possible violations of local Lorentz invariance (LLI) and local position invariance (LPI). These ...
关键词:space vehicles -- techniques: radial velocities -- gravitation 
采用多站接力跟踪策略的再入返回器定轨精度研究被引量:4
《航天器工程》2015年第5期38-43,共6页段建锋 谢剑锋 张宇 陈明 段成林 王震宇 
国家自然科学基金(11173005,11073047,11203003)
针对我国探月工程再入返回段分离前的精度要求,在无法实现对再入返回器的三向测量情况下,提出多站接力跟踪的测量策略,以解决测定轨精度不高的问题。结合再入返回分离前的测控弧段,制定两站及三站接力跟踪的策略。利用ESA"桑巴"(SAMBA)...
关键词:再入返回器 多站接力跟踪 “桑巴”卫星 定轨试验 精度分析 
通信卫星干扰源定位系统的轨道改进研究被引量:7
《宇航学报》2015年第3期330-335,共6页宋叶志 黄勇 胡小工 潘玉平 罗恒光 陈艳玲 唐成盼 
国家自然科学基金(11073047);上海市科学技术委员会(12DZ2273300);中科院行星科学重点实验室(Y386021009)
针对干扰源定位系统中通信卫星轨道误差较大问题,文章采用卫星精密定轨策略,对干扰辐射源定位系统中通信卫星的轨道改进问题进行了研究。详细研究时差与频差的测量原理,并对地球同步轨道通信卫星轨道给出了较为符合该类卫星轨道类型的...
关键词:干扰源定位 轨道确定 通信卫星 星历校正 
Orbit determination of Chang'E-3 and positioning of the lander and the rover被引量:28
《Chinese Science Bulletin》2014年第29期3858-3867,共10页Yong Huang Shengqi Chang Peijia Li Xiaogong Hu Guangli Wang Qinghui Liu Weimin Zheng Min Fan 
supported by the National Natural Science Foundation of China (11073047,11173052);the Science and Technology Commission of Shanghai (12DZ2273300);the National High Technology Research and Development Program of China (2012AA121603);the Planetary Sciences Laboratory of Chinese Academy of Sciences;the Lunar Exploration Project of China
Chang’E-3 landed on the east of Sinus Iridum area on December 14,2013,performing China’s first successful soft landing on the lunar surface.We present the results on precision orbit determination and positioning of ...
关键词:精密定轨 着陆器 月球车 定位 甚长基线干涉测量 SELENE 位置误差 相对位置 
嫦娥三号动力落月段轨迹确定策略被引量:10
《飞行器测控学报》2014年第3期236-243,共8页昌胜骐 黄勇 宋叶志 李培佳 胡小工 
国家自然科学基金(No.11073047);上海市科学技术委员会基金(No.12DZ2273300);上海市导航实验室开放课题(No.Y224353002)
针对CE-3(嫦娥三号)月球探测器动力下降弧段,特别是悬停避障段频繁机动的特点,提出了采用B样条函数逼近方法进行落月轨迹确定。仿真分析表明:在动力下降运动较平滑弧段,B样条逼近法计算结果略优于多项式拟合法;而在频繁机动弧段,B样条...
关键词:落月轨迹 B样条函数 三向测量 软着陆 嫦娥三号(CE-3) 
Precise positioning of the Chang'E-3 lunar lander using a kinematic statistical method被引量:11
《Chinese Science Bulletin》2012年第35期4545-4551,共7页HUANG Yong HU XiaoGong LI PeiJia CAO JianFeng JIANG DongRong ZHENG WeiMin FAN Min 
supported by the National Natural Science Foundation of China(11073047,10703011);Science and Technology Commission of Shanghai(12DZ2273300)
A kinematic statistical method is proposed to determine the position for Chang'E-3(CE-3) lunar lander.This method uses both ranging and VLBI measurements to the lander for a continuous arc,combing with precise knowled...
关键词:月球着陆器 精确定位 统计方法 VLBI测量 DEM数据 位置精度 数字高程模型 表面精度 
嫦娥二号再拓展试验测定轨精度研究被引量:6
《飞行器测控学报》2012年第4期84-89,共6页曹建峰 刘磊 刘勇 胡松杰 李勰 崔颖 
国家自然科学基金(11173005,11073047);863项目(2010AA122202,2011AA7034057G)
基于"嫦娥二号"卫星再拓展试验的设计轨道,研究各种摄动力对轨道确定精度的影响,得出的结论是:若要达到km量级的轨道确定精度,必须考虑除天王星和海王星之外所有大行星以及日月的质点引力。文章进一步利用数值分析法研究再拓展任务...
关键词:嫦娥二号 再拓展试验 轨道确定 协方差分析 数值仿真 
Multipath error detection and correction for GEO/IGSO satellites被引量:33
《Science China(Physics,Mechanics & Astronomy)》2012年第7期1297-1306,共10页WU XiaoLi ZHOU JianHua WANG Gang HU XiaoGong CAO YueLing 
supported by the National High Technology Research and Development Program of China (863) (Grant Nos.2009Z12A324 and 2009AA12Z328);the National Natural Science Foundation of China (Grant Nos. 10703011, 11073047 and 11033004);the Science and Technology Commission of Shanghai (Grant No. 06DZ22101)
Constellations of regional satellite navigation systems are usually constituted of geostationary satellites (GEO) and inclined geostationary satellites (IGSO) for better service availability. Analysis of real data sho...
关键词:multipath error carrier smoothing pseudorange GEO satellite position error 
Orbit determination for Chang'E-2 lunar probe and evaluation of lunar gravity models被引量:31
《Science China(Physics,Mechanics & Astronomy)》2012年第3期514-522,共9页Li PeiJia Hu XiaoGong Huang Yong Wang GuangLi Jiang DongRong Zhang XiuZhong Cao JianFeng Xin Nan 
supported by the National Natural Science Foundation of China (Grant Nos. 10703011 and11073047);the Science and Technology Commission of Shanghai (GrantNo. 06DZ22101);the National High Technology Research and Development Program of China (Grant No. 2010AA122202)
The Unified S-Band (USB) ranging/Doppler system and the Very Long Baseline Interferometry (VLBI) system as the ground tracking system jointly supported the lunar orbit capture of both Chang'E-2 (CE-2) and Chang...
关键词:Chang'E-2 VLBI orbit determination lunar gravity field 
Relative position determination of a lunar rover using the biased differential phase delay of same-beam VLBI被引量:12
《Science China(Physics,Mechanics & Astronomy)》2011年第12期2284-2295,共12页CHEN Ming LIU QingHui WU YaJun ZHAO RongBing DAI ZhiQiang 
supported by the Hundred Talent Project(s) of Chinese Academy of Sciences;the National Natural Science Foundation of China (Grant Nos.11073048 and 11073047);the Pujiang Project of Shanghai (Grant No.10PJ1411700);Shanghai Key Laboratory of Space Navigation and Position Techniques (Grant No.Y054262001)
When only data transmission signals with a bandwidth of 1 MHz exist in the rover, the position can be obtained using the differential group delay data of the same-beam very long baseline interferometry (VLBI). The rel...
关键词:same-beam VLBI biased differential phase delay relative position determination lunar rover 
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