共查询到16条相似文献,搜索用时 125 毫秒
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针对低轨卫星星座有待合理化设计的问题,深入研究了低轨卫星星座增强北斗三号系统定位性能。分析轨道高度、轨道倾角、星座构型对星座覆盖性能的影响,仿真北斗三号、GPS和3种不同类型的低轨星座,研究各低轨星座与北斗三号、GPS的组合系统在所选7个测站以及全球范围内的可见卫星数和PDOP值分布。结果表明低轨卫星对北斗三号的增强效果主要与低轨卫星数目有关,且不同轨道倾角的组合低轨星座有利于均衡系统在全球范围内的可见卫星数与PDOP值分布。低轨卫星有望通过改善卫星观测几何构型提高北斗三号系统的定位性能,且增强效果与低轨星座构型密切相关。 相似文献
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针对低轨卫星快速空间几何变化和抗干扰能力强等特征,该文基于卫星工具包软件对全球导航定位系统和铱星系统星座进行了仿真,并假定铱星具有导航卫星的功能,分析铱星对GPS定位的增强作用。首先对GPS和铱星增强星座的可见卫星数量和几何精度因子值进行了分析,然后通过对不同的误差值建模,对GPS系统和铱星系统的观测值进行了仿真,分析了低轨卫星对双差定位浮点解和模糊度固定的增强作用,结果表明:低轨卫星的加入增加了可见卫星数量,几何精度因子也优于单GPS系统。单频双差模糊度浮点解的RMS值优于1周,双频双差模糊度浮点解的RMS值优于0.5周,与单GPS相比有了较明显的提高,同时,低轨卫星的加入更有利于单频短基线的模糊度固定。 相似文献
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受限于区域监测站及地球静止轨道(geosynchronous earth orbit, GEO)卫星的静地特性,北斗卫星导航系统(BeiDou satellite navigation system,BDS)定轨精度较差,加入低轨卫星(low earth orbit,LEO)星载数据可显著提升定轨精度。使用一种由24颗LEO卫星组成的小型低轨卫星星座,在BDS-3全星座情况下,仿真分析了导航卫星与低轨卫星联合定轨对北斗卫星轨道的提升程度。分别进行仅地面测站定轨、地面测站与LEO联合定轨试验,包含全球均匀、亚太区域、亚海分布3类测站布局。结果表明:(1)仅地面测站定轨时,GEO卫星轨道三维精度在分米量级,加入LEO观测数据后,定轨精度在厘米量级,提升程度达80%以上;(2)区域地面测站时,导航卫星轨道三维精度在分米量级,加入LEO卫星后,所有类型导航卫星定轨精度均提升至数个厘米,提升效果显著;(3)全球均匀测站时,LEO的加入仍然可提升倾斜地球同步轨道/中高轨道卫星定轨精度,提升效果在毫米至厘米量级。 相似文献
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接收机自主完好性监测(receiver autonomous integrity monitoring,RAIM)是终端用户高可靠导航定位的保障,低轨卫星的发展为完好性监测带来新的机遇,然而不同低轨星座增强下的终端RAIM性能可能会存在显著差异。基于高轨道倾角(80颗)、中轨道倾角(120颗)和混合轨道倾角(168颗)3种典型的低轨星座,系统评估了低轨卫星增强下的北斗卫星导航系统(BeiDou navigation satellite system,BDS)RAIM可用性及故障检测效果。仿真计算结果表明:对于高纬区域,高轨道倾角增强下的RAIM可用性效果最好,而在中、低纬区域,中轨道倾角星座增强下的RAIM可用性效果最优;在全球范围内,高轨道倾角、中轨道倾角和混合轨道倾角星座增强下非精密进近阶段的RAIM可用性较BDS分别提升30.5%、29.0%和41.0%。由此可知,由不同轨道倾角组成的混合星座可较好地弥补可视卫星在空间覆盖上的缺陷,其全球RAIM可用性增强效果最优,增强下的RAIM可检测到的最小伪距偏差较之前平均减小33.3 m。 相似文献
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全球卫星导航定位系统是20世纪80年代出现的最具划时代意义的航天技术和信息技术,其开发和应用研究已经成为世界各大国发展战略中高技术竞争的一个主要焦点。在卫星导航系统的研究中,导航星座轨道的精密确定和预报技术是保证卫星导航系统正常运行最核心的关键技术。导航星座的轨道精度是衡量卫星导航系统性能的一个重要指标,而利用导航星座进行低轨卫星精密定轨是导航卫星应用领域的最前沿、最具战略性的方向,高精度的低轨卫星轨道是提高卫星应用水平的基础。基于星载GPS数据的低轨卫星精密定轨一直是国际上的一个研究热点,也是我国提高低轨卫星精密定轨精度的最为有效的手段,但我国还鲜有高精度成果报道。因此,加大该领域的研究力度,建立自主产权的卫星导航数据综合处理软件势在必行。 相似文献
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针对定位、导航、授时、遥感、通信一体的天基信息实时服务系统对遥感信息高时间分辨率获取的需求,提出了基于改进粒子群优化(particle swarm optimization,PSO)算法的遥感卫星星座优化设计方法。基于6N和3+4P星座构型,以重访时间间隔作为优化目标,采用改进的PSO算法对星座优化模型进行求解,分别针对全球覆盖和区域覆盖任务进行了仿真对比试验。仿真结果表明,提出的方法适用于低轨遥感卫星星座设计,满足高时间分辨率要求。 相似文献
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实现低轨导航增强的关键前提是实现低轨星座的整网时间同步,本文针对低轨导航增强系统,提出了一种基于实时精密单点定位(RT-PPP)的低轨卫星高精度时间同步方法,以解决低轨星座实时高精度时间同步的问题. 本文分析了在处理过程中存在的各类误差,介绍了低轨卫星采用状态空间(SSR)改正信息通过精密单点定位(PPP)实现实时高精度时间同步方法的处理流程,将此方法应用于气象、电离层与气候星座观测系统(COSMIC)卫星实测数据的处理,并将该方法与采用广播星历伪距的方法以及事后精密星历的方法进行了比较分析. 结果表明:采用SSR改正信息PPP的方式对2颗COSMIC卫星进行GPS双频观测值的解算,得到的轨道误差的标准差在分米级,钟差误差标准差分别在2.4 ns和2.3 ns左右,可以达到纳秒级. 通过对不同方法解算的结果进行比较可以看出,采用SSR改正信息PPP的方法明显优于采用广播星历伪距方法的解算精度,且与事后精密星历PPP的方法解算精度相当. 相似文献
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低轨道地球卫星(LEO)具有相对地面几何构型变化快、播发信号链路损耗小等优点.随着低轨卫星载荷研制与发射成本的逐渐降低,低轨卫星导航增强技术成为当前卫星导航领域的研究热点.目前国内外的低轨导航增强技术研究均处于起步阶段,没有成熟的低轨卫星导航星座,缺乏有效的低轨导航增强系统的服务性能验证手段.文中开展对低轨导航卫星轨道外推方法、低轨卫星信号捕获跟踪技术的研究,设计构建低轨导航增强系统半物理仿真平台.在仿真平台的基础上对北斗/低轨增强系统组合应用的高精度快速精密定位方法进行验证,实现了精密单点定位(PPP)的快速收敛且具有较高的内符合精度,对于低轨卫星导航增强系统的建设与应用具有一定的科学与工程价值. 相似文献
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与全球定位系统(global positioning system,GPS)不同,北斗区域卫星导航系统(BeiDou navigation satellite system,BDS)采用了5颗地球静止轨道卫星、5颗倾斜地球同步轨道卫星和4颗中圆轨道卫星的混合星座,星座分布不均匀。特殊星座决定了不同纬度地区用户的可见卫星数量和观测几何结构存在明显差异,用户的导航定位性能存在明显的纬度效应。分别从理论模型和实际观测两个方面对不同纬度地区用户的可见卫星数目、观测几何结构和导航定位性能进行较全面分析,使用了多家厂商的接收机,在不同纬度地区进行了GPS、BDS以及两系统融合定位试验。结果表明,BDS定位性能存在明显的纬度效应,即定位精度随纬度升高而降低;GPS导航定位性能没有明显的纬度效应;BDS/GPS数据融合可以减弱纬度效应,提高导航定位服务的精度和可靠性。 相似文献
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首先描述卫星覆盖的理论以及卫星星下点在地面上的轨迹规律,然后根据导航星座的特点,通过对星座基本参数特点的讨论,并在参考GPS和GLONASS星座的基础上,确定了导航星座的构成。最后,在理论上证明了最小覆盖性的条件,随着模拟实际数据进行了验证。 相似文献
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Chinese BeiDou navigation satellite system is in official service as a regional constellation with five geostationary earth orbit (GEO) satellites, five inclined geosynchronous satellite orbit (IGSO) satellites and four medium earth orbit (MEO) satellites. There are mainly two methods for precise orbit determination of the BeiDou constellation found in the current literatures. One is the independent single-system method, where only BeiDou observations are used without help from other GNSS systems. The other is the two-step GPS-assisted method where in the first step, GPS data are used to resolve some common parameters, such as station coordinates, receiver clocks and zenith tropospheric delay parameters, which are then introduced as known quantities in BeiDou processing in the second step. We conduct a thorough performance comparison between the two methods. Observations from the BeiDou experimental tracking stations and the IGS Multi-GNSS Experiment network from January 1 to March 31, 2013, are processed with the Positioning and Navigation Data Analyst (PANDA) software. The results show that for BeiDou IGSO and MEO satellites, the two-step GPS-assisted method outperforms the independent single-system method in both internal orbit overlap precision and external satellite laser ranging validation. For BeiDou GEO satellites, the two methods show close performances. Zenith tropospheric delays estimated from the first method are very close to those estimated from GPS precise point positioning in the second method, with differences of several millimeters. Satellite clock estimates from the two methods show similar performances when assessing the stability of the BeiDou on board clocks. 相似文献
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The BeiDou satellite navigation system (BDS) is different from other global navigation satellite systems (GNSSs) because of its special constellation, which consists of satellites in geostationary earth orbit, inclined geosynchronous earth orbit (IGSO), and medium earth orbit (MEO). Compared to MEO satellites, the observations of IGSO satellites cover only a small range of nadir angles. Therefore, the estimation of phase center offsets (PCOs) suffers from high correlation with other estimation parameters. We have estimated the phase center offsets for BeiDou IGSO and MEO satellites with a direct PCO parameters model, and constraints are applied to cope with the correlation between the PCOs and other parameters. Validation shows that the estimated PCO parameters could be used to improve the accuracy of orbit and clock offset overlaps. Compared with the Multi-GNSS Experiment antenna phase center correction model, the average improvements of the proposed method for along-track, cross-track, and radial components are 19 mm (31%), 5 mm (14%), and 2 mm (15%) for MEO satellites, and 13 mm (17%), 12 mm (21%), and 5 mm (19%) for IGSO satellites. For clock offset overlaps, average improvements of standard deviation and root mean square (RMS) are 0.03 ns (20%) and 0.03 ns (12%), respectively. The RMS of precise coordinates in the BDS-only positioning was also improved significantly with a level of 24 mm (30%) in the up-direction. Finally, the overall uncertainty of the estimated results is discussed. 相似文献
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中国的北斗卫星导航系统(BeiDou navigation satellite system,BDS)是全球导航卫星系统(global navigation satellite system,GNSS)中唯一全星座提供3频信号的卫星导航系统,其信号频率间共存在3种频间偏差(differential code bias,DCB),分别是DCBC2I-C7I、DCBC2I-C6I、DCBC7I-C6I。理论上,这3种DCB之间存在代数和为零的关系。基于3种频间偏差闭合差约束,加入DCB观测方程,以北斗中轨道(medium earth orbit,MEO)和倾斜地球同步轨道(inclined geosynchronous satellite orbit,IGSO)卫星作为参考卫星,采用附加限制条件的间接平差方法同步估计BDS的3种DCB。选取2018年1月1日—30日多模GNSS实验(multi-GNSS experiment,MGEX)基准站的BDS 3频数据,分别采用附加闭合差约束估计和独立求解两种方法计算北斗二代卫星的3种频间偏差。以中国科学院(Chinese Academy of Sciences,CAS)和德国宇航中心(Deutsches Zentrum für Luft- und Raumfahrt,DLR)的DCB产品作为参考,分析了所提方法估计的DCB精度、稳定性及部分典型卫星的DCB时间序列,验证了所提方法对北斗3频DCB估计的适用性和科学性,并通过BDS单频标准单点定位(standard point positioning,SPP)实验验证了DCB对单点定位精度的影响效果。 相似文献
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Improving BeiDou precise orbit determination using observations of onboard MEO satellite receivers 总被引:1,自引:0,他引:1
In recent years, the precise orbit determination (POD) of the regional Chinese BeiDou Navigation Satellite System (BDS) has been a hot spot because of its special constellation consisting of five geostationary earth orbit (GEO) satellites and five inclined geosynchronous satellite orbit (IGSO) satellites besides four medium earth orbit (MEO) satellites since the end of 2012. GEO and IGSO satellites play an important role in regional BDS applications. However, this brings a great challenge to the POD, especially for the GEO satellites due to their geostationary orbiting. Though a number of studies have been carried out to improve the POD performance of GEO satellites, the result is still much worse than that of IGSO and MEO, particularly in the along-track direction. The major reason is that the geostationary characteristic of a GEO satellite results in a bad geometry with respect to the ground tracking network. In order to improve the tracking geometry of the GEO satellites, a possible strategy is to mount global navigation satellite system (GNSS) receivers on MEO satellites to collect the signals from GEO/IGSO GNSS satellites so as that these observations can be used to improve GEO/IGSO POD. We extended our POD software package to simulate all the related observations and to assimilate the MEO-onboard GNSS observations in orbit determination. Based on GPS and BDS constellations, simulated studies are undertaken for various tracking scenarios. The impact of the onboard GNSS observations is investigated carefully and presented in detail. The results show that MEO-onboard observations can significantly improve the orbit precision of GEO satellites from metres to decimetres, especially in the along-track direction. The POD results of IGSO satellites also benefit from the MEO-onboard data and the precision can be improved by more than 50% in 3D direction. 相似文献