共查询到18条相似文献，搜索用时 125 毫秒
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根据卫星双向共视法进行时间比对的基本原理,详细介绍了Sagnac效应产生的原因。并以圆轨道地球静止同步卫星为例,推导了卫星双向共视法时间比对中Sagnac效应在地心惯性系的基本计算模型。给出了当地面站在赤道上和不在赤道上这两种情况下,Sagnac效应的详细计算过程。 相似文献
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根据卫星双向共视法进行时间比对的基本原理,详细介绍了Sagnac效应产生的原因.并以圆轨道地球静止同步卫星为例,推导了卫星双向共视法时间比对中Sagnac效应在地心惯性系的基本计算模型.给出了当地面站在赤道上和不在赤道上这两种情况下,Sagnac效应的详细计算过程. 相似文献
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结合了圆迹SAR(CSAR)和地球同步轨道SAR(GEOSAR)的特点,地球同步轨道圆迹SAR(GEOCSAR)具有大面积区域观测、可获得目标三维信息、可对目标区域连续监测等优点。但GEOCSAR合成孔径时间长,完成整个圆周孔径测量的时间为24小时,而大气变化的时间尺度经常表现为数分钟到数小时,因此大气折射率时间变化将会对GEOCSAR方位向聚焦成像产生重要影响。本文考虑L波段GEOCSAR,因此对流层和电离层效应均不可忽略。文中建立了对流层和电离层折射率时间变化引起的相位误差模型,分析和推导了折射率时间变化对GEOCSAR方位向聚焦性能的影响,计算了引起L波段GEOCSAR聚焦性能退化的最小对流层折射率和电离层电子含量随机时间变化量,并通过仿真进行了验证。 相似文献
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利用空间高精度时频系统提供的超高精度时间频率信号,可以开展一系列空地时频传递和基础物理实验,支撑相对论及相关理论的高精度检验。针对空间激光链路时频传递算法进行了理论推导及仿真分析。首先,从星地激光双向时间比对理论公式出发,对比分析了X型星地双向时间比对与Lambda型星地双向时间比对的优缺点。其次,针对空间站轨道高度讨论了相对论效应对坐标时与原时转换的影响。最后,讨论了空地时频比对数据不连续性对空间站高精度原子钟稳定性评估的影响。结果表明：(1)基于激光测距方式的Lambda型双向时间比对可以抵消一阶多普勒对上下行距离项差异的影响,且Sagnac项影响的增大可忽略;(2)星地时间比对中坐标时和原时转换的相对论项对空间站位置的速度精度提出了高要求,为实现1×10-18量级的频率偏差比对精度,空间站地心距精度要求为1 dm,速度精度要求为0.1mm/s;(3)受空间站对地可见性影响,仅利用国内测站无法通过星地链路进行中短期原子钟稳定性的评估。 相似文献
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时间同步技术是卫星导航定位系统设计的关键技术之一。根据卫星双向共视法时间比对的基本原理，详细推导了该时间同步方法在地心惯性系中精确到卫星和地面站速度的二次幂以及加速度的一次幂的计算模型，并以GEO卫星和GPS卫星为例，分析了该计算模型中的距离改正项时延对地面站间相对钟差的影响量级。结果表明：对于GEO卫星、GPS卫星与地面站之间的比对，当要求 的计算精度时，距离改正项时延只需要考虑到卫星速度项、地面站速度项的影响；当要求 的计算精度时，还需要考虑到卫星速度二次幂项、卫星加速度项、地面站与卫星相对钟差对卫星速度项、地面站间相对钟差对地面站速度项的影响。 相似文献
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谢金石 《测绘科学技术学报》2016,(5)
针对导航星座自主定轨,提出一种提高集中式算法效率的新思路,即充分利用高频、高精度的星间链路测距信息,在短弧内将卫星最优轨道与长期预报轨道的差异用多次曲线描述,得到卫星位置和速度的最佳估值。此方法无需动力学建模和计算状态转移矩阵,因此算法极为简洁。同时,对于自主运行期间缺乏空间基准,提出约束轨道升交点赤经的方法,以减小对地面系统的依赖程度。仿真结果表明,导航星座自主运行60 d,不考虑地球自转参数(EOP)长期预报误差,在无锚固站的情况下,链路数不少于5条时能够达到轨道URE优于1 m,位置3 m,速度毫米级的定轨精度。最后,通过比对验证了新算法比已有EKF分布式自主定轨算法的效率更高。 相似文献
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Reduced ARAIM monitoring subset method based on satellites in different orbital planes 总被引：2，自引：0，他引：2
With the development of the Global Navigation Satellite System, the increased number of satellites has resulted in more fault hypothesis situations and subset solutions. This situation represents a new challenge for advanced receiver autonomous integrity monitoring (ARAIM) in terms of the computational load. To efficiently detect faults and reduce the computational load, a method based on the association between satellite features in the same orbital plane is proposed. This approach first tests subsets that exclude entire constellations to narrow the search range for faults. Next, we evaluate multiple-fault cases directly by utilizing the subsets that exclude entire orbit satellites. Compared with the baseline Multiple Hypothesis Solution Separation (MHSS) method, our method can clearly reduce the number of subsets and the computational time under a typical multi-constellation situation while satisfying the localizer precision vertical 200 performance requirement, i.e., the guidance supports approach operations down to 200-foot altitudes. Furthermore, the experimental results illustrate that the number of subsets is reduced at most by two orders of magnitude, from 1330 to 87, and the computational time is decreased by 66.6%. The effective monitoring threshold and the fault-free 10?7 error bound on the accuracy of our method are much closer to those of the baseline MHSS method, and the usability coverage of both methods reaches 100%. This study verifies that the monitoring subsets and the calculation time for ARAIM are dramatically reduced by the new method. 相似文献
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插值方法是获取卫星轨道任意历元卫星坐标的重要手段,对于GNSS导航中的多轨道实时导航计算问题,进行高精度测量时需要对精密星历进行轨道插值。目前应用较为广泛的插值方法包括拉格朗日法、牛顿多项式插值以及线性逐次内维尔插值方法。本文通过研究常见的插值方法,结合具体算例进行精度及时间的对比分析,并对牛顿插值进行改进,得出结论:牛顿插值经加窗处理后卫星位置误差精度可达mm级。它的计算效率大约是拉格朗日插值及内维尔插值方法的10倍。 相似文献
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The DORIS Doppler measurements collected by Jason-1 are abnormally perturbed by the influence of the South Atlantic Anomaly (SAA). The DORIS ultra-stable oscillators on-board Jason-1 are not as stable as they should be; their frequency is sensitive both to the irradiation rate and to the total irradiation encountered in orbit. The consequence is that not only are the DORIS measurement residuals higher than they ought to be, but also large systematic positioning errors are introduced for stations located in the vicinity of the SAA. In this paper, we present a method that has been devised to obtain a continuous observation of Jason-1 frequency offsets. This method relies on the precise determination of the station frequency and troposphere parameters via the use of other DORIS satellites. More than 3 years of these observations have then been used to construct a model of response of the oscillators of Jason-1 to the SAA. The sensitivity of the Jason-1 oscillators to the SAA perturbations has evolved over time, multiplied by a factor of four between launch and mid-2004. The corrective performances of the model are discussed in terms of DORIS measurement residuals, precise orbit determination and station positioning. The average DORIS measurement residuals are decreased by more than 7 % using this model. In terms of precise orbit determination, the 3D DORIS-only orbit error decreases from 5 to 4.2 cm, but the DORIS+SLR orbit error is almost unaffected, due to the already good quality of this type of orbit. In terms of station positioning, the model brings down the average 3D mono-satellite monthly network solution discrepancy with the International Terrestrial Reference Frame ITRF2000 from 11.3 to 6.1 cm, and also decreases the scatter about that average from 11.3 to 3.7 cm. The conclusion is that, with this model, it is possible to re-incorporate Jason-1 in the multi-satellite geodetic solutions for the DORIS station network. 相似文献
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针对低轨卫星LEO星载GPS实时定轨中存在的问题,提出了以单点定位结果为观测值,采用自适应卡尔曼滤波(AKF)方法进行动力平滑来实现LEO星载GPS实时动力法定轨。采用2004-03-29~31日的GRACE-A卫星实测数据进行了实时定轨计算,并分析了自适应因子、噪声补偿方差、GPS信号中断对自适应定轨的影响。通过计算分析发现,采用AKF进行LEO星载GPS实时定轨可有效解决采用EKF噪声补偿方差难以确定的难题。同时还发现,采用AKF进行LEO星载GPS实时定轨具有较强的稳定性。 相似文献
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多系统全球导航卫星系统（Global Navigation Satellite System,GNSS）精密轨道确定及其预报是实现高精度实时精密定位的前提。针对多GNSS系统超快速轨道解算时效性及轨道预报精度随时间下降的问题,提出一种基于分块递推最小二乘配置方法,该方法通过对动力学和几何学待估参数松弛、连接以及轨道状态参数转移递推,能够同时兼容事后及实时滤波定轨方法。该方法能够有效地提高多GNSS系统轨道解算效率,缩短实时轨道更新时间。基于全球实测数据验证了该方法的可靠性和有效性,轨道精度优于国际GNSS服务组织发布的GPS超快速轨道及德国地学研究中心发布的超快速轨道,实验结果表明,采用该方法,GPS/GLONASS/Galileo/BDS四系统120个地面测站精密定轨可以实现1 h更新,延迟30 min发布,统计GPS/GLONASS/Galileo/BDS实时轨道可用部分3D均方根分别为2.8 cm、8.5 cm、5.0 cm及11.5 cm（IGSO/MEO）。目前,1 h更新多GNSS系统轨道及实时产品服务系统已业务化发布,较之前发布的3 h更新及6 h更新轨道分别有20%~40%的精度提升。 相似文献
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Exploring gravity field determination from orbit perturbations of the European Gravity Mission GOCE 总被引：5，自引：0，他引：5
A comparison was made between two methods for gravity field recovery from orbit perturbations that can be derived from global
positioning system satellite-to-satellite tracking observations of the future European gravity field mission GOCE (Gravity
Field and Steady-State Ocean Circulation Explorer). The first method is based on the analytical linear orbit perturbation
theory that leads under certain conditions to a block-diagonal normal matrix for the gravity unknowns, significantly reducing
the required computation time. The second method makes use of numerical integration to derive the observation equations, leading
to a full set of normal equations requiring powerful computer facilities. Simulations were carried out for gravity field recovery
experiments up to spherical harmonic degree and order 80 from 10 days of observation. It was found that the first method leads
to large approximation errors as soon as the maximum degree surpasses the first resonance orders and great care has to be
taken with modeling resonance orbit perturbations, thereby loosing the block-diagonal structure. The second method proved
to be successful, provided a proper division of the data period into orbital arcs that are not too long.
Received: 28 April 2000 / Accepted: 6 November 2000 相似文献
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针对GPS、SLR和DORIS三种不同手段的各自定轨精度问题,本文基于不同的轨道评估方法进行了深入分析。以JASON-2卫星为例,分析了姿态模型误差及其对定轨精度的影响,分别讨论了GPS、SLR和DORIS的定轨策略和定轨精度,并基于轨道评估结果进行了轨道叠加。基于实测数据进行了试验,试验结果表明,JASON-2卫星姿态模型误差对DORIS、GPS和SLR轨道影响分别为0.040、0.036和0.033m;DORIS定轨结果优于GPS和SLR,SLR定轨精度最差;基于SLR验证和轨道重叠结果加权,对GPS、SLR和DORIS轨道进行轨道叠加,其精度一致,通过与JPL轨道比较,其径向精度为2cm。 相似文献