|
|
|
题名
|
作者
|
年代
|
出处
|
被引量
|
| 1 | Orbit determination and time synchronization for a GEO/IGSO satellite navigation constellation with regional tracking network显示文摘Aiming at regional services,the space segment of COMPASS (Phase I) satellite navigation system is a constellation of Geostationary Earth Orbit (GEO),Inclined Geostationary Earth Orbit (IGSO) and Medium Earth Orbit (MEO) satellites.Precise orbit determination (POD) for the satellites is limited by the geographic distribution of regional tracking stations.Independent time synchronization (TS) system is developed to supplement the regional tracking network,and satellite clock errors and orbit data may be obtained by simultaneously processing both tracking data and TS data.Consequently,inconsistency between tracking system and TS system caused by remaining instrumental errors not calibrated may decrease navigation accuracy.On the other hand,POD for the mixed constellation of GEO/IGSO/MEO with the regional tracking network leads to parameter estimations that are highly correlated.Notorious example of correlation is found between GEO's orbital elements and its clock errors.We estimate orbital elements and clock errors for a 3GEO+2IGSO constellation in this study using a multi-satellite precise orbit determination (MPOD) strategy,with which clock error elimination algorithm is applied to separate orbital and clock estimates to improve numerical efficiency.Satellite Laser Ranging (SLR) data are used to evaluate User Ranging Error (URE),which is the orbital error projected on a receiver's line-of-sight direction.Two-way radio-wave time transfer measurements are used to evaluate clock errors.Experimenting with data from the regional tracking network,we conclude that the fitting of code data is better than 1 m in terms of Root-Mean-Square (RMS),and fitting of carrier phase is better than 1 cm.For orbital evaluation,difference between computed receiver-satellite ranging based on estimated orbits and SLR measurements is better than 1 m (RMS).For clock estimates evaluation,2-hour linear-fitting shows that the satellite clock rates are about 1.E-10 s/s,while receiver clock rates are about 1×10 13-1×10 12 s/s.For the 72-hour POD experiment,the average differences between POD satellite clock rates estimates and clock measurements based on TS system are about 1×10 13 s/s,and for receiver clock rates,the differences are about 1×10 15 s/s. | ZHOU ShanShi HU XiaoGong WU Bin LIU Li QU WeiJing GUO Rui HE Feng CAO YueLing Wu XiaoLi ZHU LingFeng SHI Xin TAN HongLi | 2011 | Science China(Physics,Mechanics & Astronomy)2011，54，6： | 44 |
| 2 | 北斗三号卫星两种定轨模式精度比较分析显示文摘北斗全球卫星导航系统(BDS-3)已经于2018年年底建成基本系统,并计划于2020年建成完整系统,而精确的卫星轨道是实现高性能全球服务的前提。本文基于北斗三号基本系统的18颗中圆轨道(MEO)卫星,评估了北斗三号卫星星间链路的测量噪声与测距精度,利用中国境内12个区域监测站的星地观测和星间链路观测,进行了联合卫星轨道测定试验,并与单纯区域监测站观测定轨结果进行了比较,分析了两种定轨模式重叠弧段轨道误差、轨道预报精度和激光检核精度。结果表明:北斗三号卫星的星间链路测量噪声为2.9cm,测距精度约为4.4cm;仅采用区域测站定轨,重叠弧段三维位置误差RMS为66.7cm,加入星间链路后可降低至15.4cm,提高了76.9%,24h轨道预报位置精度也由114.1cm提升至20.3cm,提升了83.2%,激光检核径向精度为8.4cm左右,明显优于北斗二号卫星轨道精度。 | 杨宇飞 杨元喜 胡小工 唐成盼 赵立谦 徐君毅 | 2019 | 测绘学报2019，48，7： | 26 |
| 3 | Improvement of orbit determination for geostationary satellites with VLBI tracking显示文摘China’s COMPASS satellite navigation system consists of five or more geostationary (GEO) satellites.The roles of GEO satellites are to improve the regional user’s positioning accuracy and provide the continuous Radio Determination Satellite Service.The motion of GEO satellites relative to a ground tracking station is almost fixed,and regular orbit maneuvers are necessary to maintain the satellites’ allocated positions above the equator.These features present difficulties in precise orbit determination (POD).C-band ranging via onboard transponders and the L-band pseudo-ranging technique have been used in the COMPASS system.This paper introduces VLBI tracking,which has been successfully employed in the Chinese lunar exploration programs Chang’E-1 and Chang’E-2,to the POD of GEO satellites.In contrast to ranging,which measures distances between a GEO satellite and an observer,VLBI is an angular measurement technique that constrains the satellite’s position errors perpendicular to the satellite-to-observer direction.As a demonstration,the Chinese VLBI Network organized a tracking and orbit-determination experiment for a GEO navigation satellite lasting 24 h.This paper uses the VLBI delay and delay-rate data,in combination with C-band ranging data,to determine the GEO satellite’s orbit.The accuracies of the VLBI delay and delay rate data are about 3.6 ns and 0.4 ps/s,respectively.Data analysis shows that the VLBI data are able to calibrate systematic errors of the C-band ranging data,and the combination of the two observations improves orbit prediction accuracy with short-arc data,which is important for orbital recovery after maneuvers of GEO satellites.With the implementation of VLBI2010,it is possible for VLBI to be applied in the COMPASS satellite navigation system. | HUANG Yong HU XiaoGong ZHANG XiuZhong JIANG DongRong GUO Rui WANG Hong SHI ShanBin | 2011 | Chinese Science Bulletin2011，56，26： | 18 |
| 4 | GEO and IGSO joint precise orbit determination显示文摘Experiments and analyses are carried out for GEO and joint GEO/IGSO precise orbit determination using data recorded by China's regional tracking network.Results show that joint GEO/IGSO orbit determination effectively solves the problem of poor observation geometry for GEO satellites.The laser radial evaluation thus confirms that precision is as good as less than 0.1 m.In the case of joint orbit determination,solving the empirical acceleration can reduce errors introduced by the imprecise solar radiation pressure model used for Chinese satellites.This method also improves the accuracy of orbit prediction in the radial direction.The ephemeris accuracy is thus improved and the ephemeris can provide a better service to users with navigation and positioning requirements. | MAO Yue DU Yu SONG XiaoYong JIA XiaoLin WU XianBing | 2011 | Science China(Physics,Mechanics & Astronomy)2011，54，6： | 14 |
| 5 | 风云3C增强北斗定轨试验结果与分析显示文摘首次搭载GPS/BDS双模接收机全球导航卫星掩星探测仪(GNOS)的风云三号C星于2013年9月23日的成功发射,为研究低轨卫星对BDS定轨增强提供了便利。本文首先对低轨卫星GNOS搭载的GPS/BDS双模接收机的观测数据进行统计,并分析了伪距测量精度。然后在全球测站、区域测站两种布局情况下,对无GNOS的BDS单系统定轨、无GNOS的GPS/BDS双系统定轨、有GNOS的BDS单系统定轨增强、有GNOS的GPS/BDS双系统定轨增强4种方案进行北斗轨道及钟差比较分析。结果表明,GNOS对北斗卫星轨道增强在全球测站下,GEO卫星切向精度提升最为显著,提升程度达60%,其次是法向和其他类型卫星切向,部分弧段个别GEO卫星径向精度稍有下降。双系统定轨增强中可视弧段钟差重叠精度RMS值有0.1ns量级改善。7个国内测站区域监测网的定轨试验中对轨道进行了预报,结果表明GNOS对北斗GEO卫星轨道预报精度切向提升达85%,其余方向及卫星有较大改善,平均21.7%。可视弧段钟差重叠精度RMS值有0.5ns量级改善。 | 曾添 隋立芬 贾小林 计国锋 张清华 | 2017 | 测绘学报2017，46，7： | 11 |
| 6 | Results and Analyses of BDS Precise Orbit Determination with the Enhancement of Fengyun-3C显示文摘Global navigation satellite system occultation sounder (GNOS) Fengyun-3C was launched successfully on September 23, 2013, which carried GPS/BDS receiver for the first time. This provides the convenience to study the enhancement results of low earth orbiter satellite (LEO) to BDS precise orbit determination (POD). First the data characteristic and code observation noise of GNOS are analyzed. Then the enhancement experiments in the case of global and regional ground observation stations layout are processed with four POD schemes: BDS single system, GPS/BDS double system, BDS single system with GNOS observations, GPS/BDS double system with GNOS observations. The precision of BDS orbits and clocks are compared via overlapping arcs. Results show that in the case of global station layout the along directional precision of GEO satellite has the biggest improvement, with the improvement percentage 60%. Then the precision of cross direction and the along direction of remaining satellites shows the second biggest improvement. The orbit precision of BDS-only POD in part of observation arcs some satellite even suffers a slight decline. The root mean square (RMS) of overlapping clock difference of visible arcs in GPS/BDS POD experiments improves by 0.1 ns level. As to the experiments of regional station layout with 7 ground stations, the orbit and clock overlapping precision and orbit predicting precision are analyzed. Results show that the predicting precision of BDS GEO satellites in the along direction improves by 85%. The remaining also has a substantial improvement, with the average percentage 21.7%. RMS of overlapping clock difference of visible arcs improves by 0.5 ns level. | Tian ZENG Lifen SUI Xiaolin JIA Guofeng JI Qinghua ZHANG | 2019 | Journal of Geodesy and Geoinformation Science2019，2，3： | 9 |
| 7 | Orbit determination and prediction for Beidou GEO satellites at the time of the spring/autumn equinox显示文摘Geostationary(GEO) satellites form an indispensable component of the constellation of Beidou navigation system(BDS). The ephemerides, or predicted orbits of these GEO satellites(GEOs), are broadcast to positioning, navigation, and timing users. User equivalent ranging error(UERE) based on broadcast message is better than 1.5 m(root formal errors: RMS) for GEO satellites. However, monitoring of UERE indicates that the orbital prediction precision is significantly degraded when the Sun is close to the Earth's equatorial plane(or near spring or autumn Equinox). Error source analysis shows that the complicated solar radiation pressure on satellite buses and the simple box-wing model maybe the major contributor to the deterioration of orbital precision. With the aid of BDS' two-way frequency and time transfer between the GEOs and Beidou time(BDT, that is maintained at the master control station), we propose a new orbit determination strategy, namely three-step approach of the multi-satellite precise orbit determination(MPOD). Pseudo-range(carrier phase) data are transformed to geometric range(biased geometric range) data without clock offsets; and reasonable empirical acceleration parameters are estimated along with orbital elements to account for the error in solar radiation pressure modeling. Experiments with Beidou data show that using the proposed approach, the GEOs' UERE when near the autumn Equinox of 2012 can be improved to 1.3 m from 2.5 m(RMS), and the probability of user equivalent range error(UERE)<2.0 m can be improved from 50% to above 85%. | LI XiaoJie ZHOU JianHua HU XiaoGong LIU Li GUO Rui ZHOU ShanShi | 2015 | Science China(Physics,Mechanics & Astronomy)2015，58，8： | 8 |
| 8 | Analysis of RDSS positioning accuracy based on RNSS wide area differential technique显示文摘The BeiDou Navigation Satellite System(BDS) provides Radio Navigation Service System(RNSS) as well as Radio Determination Service System(RDSS).RDSS users can obtain positioning by responding the Master Control Center(MCC) inquiries to signal transmitted via GEO satellite transponder.The positioning result can be calculated with elevation constraint by MCC.The primary error sources affecting the RDSS positioning accuracy are the RDSS signal transceiver delay,atmospheric trans-mission delay and GEO satellite position error.During GEO orbit maneuver,poor orbit forecast accuracy significantly impacts RDSS services.A real-time 3-D orbital correction method based on wide-area differential technique is raised to correct the orbital error.Results from the observation shows that the method can successfully improve positioning precision during orbital maneuver,independent from the RDSS reference station.This improvement can reach 50% in maximum.Accurate calibration of the RDSS signal transceiver delay precision and digital elevation map may have a critical role in high precise RDSS positioning services. | XING Nan SU RanRan ZHOU JianHua HU XiaoGong GONG XiuQiang LIU Li HE Feng GUO Rui REN Hui HU GuangMing ZHANG Lei | 2013 | Science China(Physics,Mechanics & Astronomy)2013，56，10： | 6 |
| 9 | 北斗三号星座拟稳钟差测定及其预报显示文摘北斗三号卫星搭载了Ka波段星间链路载荷,可实现卫星之间的测距与通信。将星座内所有卫星的原子钟视为一个钟组,利用星间双向观测实时测量钟组内部时差,选取部分较为稳定的钟作为基准钟,可以建立星座拟稳原子时,得到各卫星的星座拟稳钟差,再通过少量链路向BDT溯源,即可最终得到卫星相对于BDT的钟差。以星座拟稳时间为观测量进行星载原子钟性能及钟差预报精度分析,可以避免卫星轨道误差对于钟差的影响,得到更加真实可靠的分析结果。试验结果表明:北斗三号星载原子钟,尤其是氢原子钟,具有良好的稳定性,MEO卫星氢原子钟天稳哈达马方差为3.5E-15,IGSO卫星氢原子钟为2.8E-15,铷原子钟为8.2E-15;星座拟稳钟差1 h预报误差RMS约为0.1 ns,可有效分离钟差预报误差和时间溯源误差,使北斗三号空间信号精度达到甚至优于15 cm。显然,星间链路的巨大潜力有待进一步挖掘。 | 杨宇飞 杨元喜 陈金平 唐成盼 李冲 郭海荣 杨建华 刘金获 杨斌 | 2021 | 测绘学报2021，50，12： | 6 |
| 10 | 北斗卫星轨道预报精度分析及改进显示文摘针对北斗GEO、IGSO、MEO的3种卫星类型和动态偏航、零偏航两种姿态控制模式,进行了以ECOM光压模型为基础的轨道预报精度分析。确定了北斗3类卫星的短期、中期、长期预报光压参数选择策略。采用光压参数修正法,通过对北斗卫星光压参数长期变化规律建模,有效提升了地影段轨道长期预报精度。研究结果可同时服务于北斗卫星轨道确定及历书参数生成。 | 毛悦 宋小勇 胡小工 贾小林 | 2017 | 测绘科学技术学报2017，34，2： | 5 |
| 11 | 一种新的卫星导航星间链路测距体制及其定轨性能分析显示文摘现有的GPS星间链路轮询时分测距体制未针对定轨性能进行优化。对轮询时分测距体制进行改进,提出了一种新的分组时分测距体制,通过对整星座所有卫星进行分组测距来提高星间测距链路数量,从而提高星地星间联合定轨精度。以整星座平均定轨精度最优为目标,提出了两步优化算法,得到星间总测距链路数最多的卫星分组,使每组内卫星的星间测距DOP值最小。仿真结果表明,采用优化算法得到的最优分组时分测距方式对卫星定轨精度有明显改善。 | 王东会 徐博 刘文祥 孙广富 | 2014 | 国防科技大学学报2014，36，1： | 3 |
| 12 | 北斗广播电文钟差模型精度评估及改善策略显示文摘星载原子钟是北斗卫星导航系统(BDS)的核心设备,其钟差模型是北斗广播电文的重要组成部分,模型精度直接影响BDS的服务性能。本文采用星地双向时频传递(TWSTF)钟差测量为参考,评估了BDS广播电文钟差模型精度,结果表明BDS广播电文钟差模型精度优于2 ns(数据龄期小于12 h)。针对BDS广播电文钟差参数解算问题,结合BDS地面段的钟差模型解算策略,本文提出进一步提升精度的多种策略。对于1 h时长的短期预报,本文提出加权线性模型与混合区间线性模型的钟差拟合预报方法,短期预报精度可提高20%以上;对于预报时长大于6 h的中长期预报,本文采用谱分析钟差时间序列,并根据谱分析结果构造预报模型,与简单的二次多项式模型预报相比,预报6 h精度提高13%,预报12 h平均提高了21%;对于IGSO/MEO卫星,本文提出将TWSTF的设备时延值作为参数估算,使钟差模型在设备切换后精度提高18%。最后,利用本文提出的改进策略对2017年1月—6月的钟差数据重新处理,获得了新的广播电文钟差模型时间序列。利用新的广播电文钟差模型进行北斗监测接收机定位,结果表明,N、E、U 3个方向精度分别提高14.22%、29.39%、14.91%,显著提升了BDS广播电文钟差服务性能。 | 巩秀强 袁俊军 胡小工 王彬 陈俊平 周善石 | 2021 | 测绘学报2021，50，2： | 3 |
| 13 | 不同姿态控制模式下的北斗卫星定轨策略研究显示文摘北斗卫星的姿态控制分为动态偏置、零偏置和连续动偏3种,不同类型卫星、不同姿态控制模式、不同时段下定轨精度不一致,影响了北斗系统的连续性。详细研究了北斗不同类型卫星在不同姿态控制模式下的最优定轨策略,并基于实测数据进行试验,结果表明,BeiDou-2 IGSO(inclined geosynchronous orbit)/MEO(medium earth orbit)卫星采用基于星地钟差约束下多星定轨方法和ECOM(extended CODE model)5参数模型相结合的方法定轨精度最优,零偏期间,用户等效距离误差值为2.08 m,全球激光评估轨道视向精度约为1 m;BeiDou-3 IGSO/MEO卫星采用常规多星定轨和ECOM 5参数模型相结合的方法定轨精度最优;连续动偏期间,用户等效距离误差值为1.22 m,全球激光评估轨道视向精度为0.23 m,与动偏期间精度一致;GEO(geostationary earth orbit)卫星在春秋分附近时段采用基于星地钟差约束下多星定轨方法和ECOM 9参数模型相结合的方法定轨精度最优,用户等效距离误差值为0.72 m。 | 李晓杰 郭睿 吴杉 常志巧 刘帅 陈建兵 | 2019 | 武汉大学学报(信息科学版)2019，44，10： | 3 |
| 14 | Analysis of the characteristics of the harmonics coefficient J_2 of the Earth's gravity field in different periods显示文摘The characteristics of the geopotential coefficient J2 in different periods are analyzed using satellite laser ranging data spanning the last 27 years.The satellites used in the analysis are Lageos1 and Lageos2.The variations in J2 are obtained by determining the dynamic orbit.The results show that there are strong seasonal and long-term variations.For different data spans,the seasonal variations agree well in terms of both amplitude and phase.Using all the data,the amplitude and phase of the annual term are 2.5 10-10 and 127°,respectively,while the amplitude and phase of the semiannual term are 0.94 10-10 and 213°,respectively.In the case of long-term variation,the secular variation in J2(J2) is-2.2 10-11 a-1 from 1984 to 2010.J2 differs for the different periods because of interannual variations,such as the '1998 anomaly'.Another anomaly may have taken place during 2007-2010.Although the cause of the anomaly is unknown,it is an important observational constraint on the shape of the Earth. | QU WeiJing WU Bin | 2012 | Chinese Science Bulletin2012，57，14： | 2 |
| 15 | 基于中继测量的环月探测器定轨能力分析显示文摘嫦娥四号月球探测拟首次实现月球背面的软着陆,测控与数传依赖地月L2平动点的中继卫星,并有望获取四程测量与星间测量数据。对基于中继测量的环月探测器测定轨能力进行了仿真分析,结果表明,中继卫星可较好地实现环月探测器连续跟踪;在定轨能力方面,中继卫星自身轨道精度是制约环月探测器定轨精度的重要因素,当跟踪弧段达到5h以上时,定轨精度趋于稳定,但轨道精度较中继卫星的轨道精度相差1个量级;对于星间链路测量,除中继卫星自身的轨道精度外,星钟的稳定性是制约定轨精度的另一个重要因素,如果辅助以每天1h的地基跟踪亦可实现优于百m的定轨精度。 | 曹建峰 刘磊 刘也 苏伟钢 胡松杰 | 2017 | 飞行器测控学报2017，36，2： | 2 |
| 16 | 地面大功率干扰源对导航星座星间链路的干扰分析显示文摘为了定量分析地面大功率干扰源对导航星座星间链路的影响程度,提出单星干扰解析模型,通过等效载噪比定量描述干扰强度,通过测距误差和通信误码率衡量干扰对单颗导航卫星的影响。根据导航星间链路的工作特点,对卫星受干扰导致整星座星地联合定轨及星间转发通信功能异常的原理进行分析。研究结果表明:星间链路系统具有较强的抗地面干扰的能力,地面单个大功率干扰源对星地联合定轨精度的影响小于厘米级,对星间转发通信的影响仅为部分卫星的链路传输代价增加以及直接干扰卫星一段时间内的通信异常。 | 王东会 徐博 刘文祥 孙广富 | 2015 | 中南大学学报(自然科学版)2015，46，7： | 0 |
您所在的机构暂未开通此部分的功能，请联系管理员