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1.
中高轨卫星广播星历精度分析   总被引:17,自引:0,他引:17  
GPS广播星历参数具有物理意义明确、参数少、精度高等优点,可以考虑将它应用于其他卫星导航系统。但是GPS系统的卫星构成比较单一,而其他卫星导航系统可能包含中地球轨道 (MEO)、倾斜地球同步轨道(IGSO)和地球静止轨道(GEO)等多种不同类型的中高轨卫星。分析了采用GPS广播星历参数时,MEO、IGSO和GEO卫星的广播星历拟合精度,特别讨论了轨道倾角接近于0的GEO卫星的广播星历拟合精度,并给出了相应的改进措施。计算表明,对于 MEO卫星,2 h的广播星历拟合精度(三维位置)可达厘米级;对于IGSO卫星和轨道倾角较大的GEO卫星,4 h的广播星历拟合精度约为0.1 m,径向位置误差在厘米量级;而对于轨道倾角接近于0的GEO卫星,若不采取特殊措施,由于轨道倾角和升交点经度统计相关,其广播星历拟合精度很差,为此提出了一种坐标转换方法。采用此方法后的广播星历拟合精度可达0.1 m,径向位置误差为厘米量级。  相似文献   

2.
As the most sensitive single-dish radio telescope,the Five-hundred Aperture Spherical radio Telescope(FAST)is very susceptive to radio frequency interference(RFI)from active radio services.Moreover,due to the rapid development of space applications and research,satellite interference has become one of the main RFI sources for FAST,particularly at the L band.Therefore,we have developed several measures to mitigate satellite RFI.On the one hand,an antenna with 4.5-meter diameter has been constructed and installed at the FAST site to detect the satellite interference in the frequency band between 1 to 5 GHz.Meanwhile,we have developed a satellite RFI database based on the FAST sky coverage,the observing frequency bands,and known satellite systems.By combining the satellite RFI monitoring antenna and the database,we have established a satellite RFI mitigation system.With this system,we can not only track satellites to collect their characteristics and update the database but also help the observer to program the observing plan by predicting satellite interference.During the practical observation of FAST at the L band,the feasibility of this system to mitigate satellite RFI has been proved.In particular,the system effectively avoids strong satellite interference from entering the main beam of the telescope and causing receiver saturation.  相似文献   

3.
本项目组于1993年7月至8月,对青藏高原的地壳运动进行第1期监测,并用广播星历进行解算.1994年秋,又使用经武汉测绘科技大学改进到微机上的美国麻省理工学院研制的GAMIT精密定位软件和NGS(NationalGeodeticSurvey)精密星历,重新进行解算.解算结果表明,在400多公里范围内,观测两个时段平均基线的重复性达到几毫米的高精度,相对精度优于3.10×10(-8),与广播星历解相比,基线重复精度提高了5~12倍.  相似文献   

4.
The Chinese Area Positioning System (CAPS) is a positioning system based on satellite communication that is fundamentally different from the 3"G" (GPS, GLONASS and GALILEO) systems. The latter use special-purpose navigation satellites to broadcast navi-gation information generated on-board to users, while the CAPS transfers ground-generated navigation information to users via the communication satellite. In order to achieve accurate Positioning, Velocity and Time (PVT), the CAPS employs the following strategies to over-come the three main obstacles caused by using the communication satellite: (a) by real-time following-up frequency stabilization to achieve stable frequency; (b) by using a single carrier in the transponder with 36 MHz band-width to gain sufficient power; (c) by incorporating Decommissioned Geostationary Orbit communication satellite (DGEO), barometric pressure and Inclined Geostationary Orbit communication satellite (IGSO) to achieve the 3-D posi-tioning. Furthermore, the abundant transponders available on DGEO can be used to realize the large capacity of communication as well as the integrated navigation and communication. With the communication functions incorporated, five new functions appear in the CAPS: (1) combination of navigation and communication; (2) combination of navigation and high accu-racy orbit measurement; (3) combination of navigation message and wide/local area differen-tial processing; (4) combination of the switching of satellites, frequencies and codes; and (5) combination of the navigation message and the barometric altimetry. The CAPS is thereby labelled a PVT5C system of high accuracy. In order to validate the working principle and the performance of the CAPS, a trial system was established in the course of two years at a cost of about 20 million dollars. The trial constellation consists of two GEO satellites located at E87.5°and E110.5°, two DGEOs located at E130° and E142°, as well as barometric altimetry as a virtual satellite. Static and dynamic performance tests were completed for the Eastern, the Western, the Northern, the Southern and the Middle regions of China. The evaluation results are as follows: (1) land static test, plane accuracy range: C/A code, 15~25 m; P code, 5~10 meters; altitude accuracy range, 1~3 m; (2) land dynamic test, plane accuracy range, C/A code, 15~25 m; P code, 8~10m; (3) velocity accuracy, C/A code, 0.13~0.3 ms-1, P code, 0.15~0.17m s-1; (4) timing accuracy, C/A code, 160ns, P code, 13 ns; (5) timing compared accuracy of Two Way Satellite Time and Frequency Transfer (TWSTFT), average accuracy, 0.068 ns; (6) random error of the satellite ranging, 10.7 mm; (7) orbit determination accuracy, better than 2 m. The above stated random error is 1σ error. At present, this system is used as a preliminary operational system and a complete system with 3 GEO, 3 DGEO and 3 IGSO is being established.  相似文献   

5.
导航系统的完好性关系到用户的安全问题,空间信号精度(SISA)是反映卫星导航系统完好性的重要指标之一。针对导航电文中的广播星历和钟差参数信息处理问题,设计了SISA参数计算方法;利用GPS和BDS系统中的实际数据,分析了不同轨道类型卫星SISA参数对空间信号误差的包络特性,并将导航电文中URA参数与SISA参数进行比较,验证了SISA参数计算方法。实验结果表明,SISA能够准确反映广播星历的空间信号精度,并能够对空间信号误差基本实现平均98%的包络能力;目前北斗广播星历中的URA参数不能够精确反映空间信号的精度,不同卫星的空间信号精度相差较大,SISA能够准确反映和包络北斗空间信号误差。  相似文献   

6.
北斗卫星导航系统SISURE初步评估   总被引:2,自引:0,他引:2  
北斗导航系统自2018年12月27日提供全球服务以来,其服务性能受到了极大关注.以上海天文台iGMAS (International GNSS MonitoringAssessment System)分析中心发布的精密轨道、钟差产品作为基准,评估了2019年年积日3–12 d的北斗二号、北斗三号以及GPS广播星历的轨道、钟差和空间信号用户测距误差(Signal in Space User Ranging Error, SISURE,简称为URE),并且对北斗卫星导航系统结果进行了详细的分析.结果表明:在评估时间段内,北斗三号广播星历轨道精度、URE均明显优于北斗二号,且部分结果优于GPS.北斗三号广播星历轨道径向精度最高,优于0.2 m.北斗三号全部卫星URE均值优于0.4 m, URE RMS (root mean square)优于0.5 m.北斗二号每颗卫星URE均值、95%URE (置信度为95%的URE)、URE RMS小于2 m,北斗三号每颗卫星URE均值、95%URE、URE RMS小于1 m,均达到了系统公开承诺的服务性能标准.  相似文献   

7.
本文介绍了利用GPS卫星广播星历表计算卫星的坐标和速度的一种方法,这种方法可以消除广播星历中的随机噪声,使卫星的坐标精度达到广播星历应有的精度。同时卫星速度的精度也可达到相当于坐标精度的水平。  相似文献   

8.
The DArk Matter Particle Explorer(DAMPE) can measure γ-rays in the energy range from a few GeV to about 10 TeV.The direction of each γ-ray photon is reconstructed in the DAMPE payload reference system.To convert this to celestial coordinates,we require the celestial orientation of the payload system,which,however,may slightly deviate from that of the satellite system provided by the star-tracker.In this paper,we adopt a maximum likelihood method and use the γ-rays centered around several bright point-like sources to measure and correct the angular deviations between the DAMPE payload and satellite system,the so-called "boresight alignment".We also check our method of boresight alignment for some sets of simulation data with artificial orientations and obtain consistent results.The time-dependent boresight alignment analysis does not show evidence for significant variation of the parameters.  相似文献   

9.
近年来,随着GNSS (global navigation satellite system)技术的发展,利用地基和空基GNSS电离层探测的空间特征,形成了更加完善的三维电离层观测系统,获得了丰富的多源GNSS电离层观测数据,促进了电离层在理论模型、经验模型及同化模型方面的进展,同时,通过结合中性大气及等离子层等方面的...  相似文献   

10.
目前,越来越多的低轨卫星上都搭载了用于精密定轨的星载GPs接收机,星载GPS已成为低轨卫星精密定轨的主要手段之一.星载GPS精密定轨精度依赖于GPS星历及钟差精度.基于SHORDE-Ⅲ非差动力学定轨功能,以2005年8月1日至8月7日一周的GRACE卫星实测数据为例,采用事后精密轨道(igs)、快速轨道(igr)和超快速轨道(igu)三种GPS星历在同等条件下定轨,估计GPS星历精度对低轨卫星定轨精度的影响,实际计算结果表明igs和igr两类GPS星历定轨精度相当,约为9.5 cm,igu星历定轨精度略低于igs和igr星历,约为10.5cm:高频GPS卫星钟差数据对定轨精度会产生1-6cm影响.  相似文献   

11.
详细地叙述了国际空间大地测量技术服务组织ILRS(International Laser Ranging Service),IVS(International VLBI Service),IGS(International GNSS Service)和IDS(International DORIS Service)分别采用SLR(satellite laser ranging),VLBI(very long baseline interferometry),GPS(global positioning system)和DORIS(Doppler orbitography and radio-positioning intergrated by satellite)四种技术,并由多家分析中心的站坐标和地球定向参数的SINEX(solution in independent exchange format)周解(或24 h观测解)进行技术内综合解算的方法,包括技术内综合模型的建立、参考架基准约束问题和不同分析中心解的定权方法等主要内容,并对ILRS,IVS,IGS和IDS提供的技术内综合周(日)解的长期序列进行了站坐标和地球定向参数(earth orientation parameters,EOP)的精度评估,分析了地球参考架基准参数的长期特性。由地球参考架基准定义可知,SLR技术内SINEX综合解相对于ITRF2014的平移参数时间跨度最长,且没有明显的偏差或漂移;GPS技术的三个方向平移参数虽然弥散度最低,但是在X方向和Y方向存在长期的线性变化,在Z方向存在跳变;DORIS技术也有类似GPS技术的现象。这些结果说明ITRF2014选择SLR定义的地心作为参考架原点是有道理的。通过分析台站坐标精度可知,利用各种技术对核心站和非核心站进行区分非常重要,所分别得到的精度有明显的不同。由于GNSS(global navigation satellite system)台站多且分布广,因此地球定向参数的确定精度要高于其他三种技术。  相似文献   

12.
SLR新星历及其在卫星预报中的应用   总被引:1,自引:0,他引:1  
目前卫星激光测距(SLR)中所采用的IRV星历已经使用了近20年,近几年来随着对高轨卫星的测距和卫星白天测距的开展以及考虑到今后激光测距技术的发展,需要对SLR所采用的星历进行改进,以适应SLR发展的需求。从2006年8月起国际激光测距网(ILRS)将使用一种新的可用于多种目标测距的星历——CPF星历,该星历不仅可用于人造卫星的激光测距,而且还可用于月球及其转发器等目标的激光测距。该文介绍了这种SLR新星历和应用它进行卫星位置台站预报的情况,分析了其预报精度。  相似文献   

13.
与其他卫星导航系统不同,北斗卫星导航系统采用星地双向时间比对技术,直接测量卫星钟相对于地面保持的系统时间的钟差,并用于广播电文钟差参数的建模。讨论了电离层延迟误差、卫星相位中心误差等不同误差源对不同类型卫星双向时间同步卫星钟差精度的影响。实测数据分析结果表明,星地双向卫星钟差内符合精度(RMS)优于0.15 ns。利用双向卫星钟差序列,对广播星历钟差参数预报精度进行了分析,统计结果显示广播电文钟差参数预报1 h,精度在2 ns以内,移动卫星刚入境时,钟差参数预报6 h误差可达10 ns。  相似文献   

14.
The Solar Upper Transition Region Imager(SUTRI) focuses on the solar transition region to achieve dynamic imaging observation of the upper transition region. In this paper, we report the optical system design, mechanical design, ultrasmooth mirror manufacture and measurement, EUV multilayer film coating, prelaunch installation and calibration for the SUTRI payload at IPOE, Tongji University. Finally, the SUTRI carried by the SATech-01satellite was successfully set to launch. All functions of thi...  相似文献   

15.
区域北斗星基增强系统提供等效钟差改正数统一修正星历和钟差误差。随着系统的建设发展,新一代北斗星基增强系统将区分星历和钟差误差改正信息,以提高差分改正精度。由于北斗卫星混合星座设计及区域监测网的局限,星历和钟差误差的高精度分离计算面临着新的挑战。对北斗星基增强系统的星历和钟差改正算法进行了研究,分别采用动力学和运动学模式计算了卫星星历和钟差改正数,并基于北斗实测数据,对两种处理模式的差分改正精度进行了对比研究。试验结果表明,采用动力学和运动学差分方法,得到的双频伪距实时定位精度分别为1.76m和1.78m,定位精度与WAAS及EGNOS相当。利用运动学和动力学差分改正数后均可得到分米级的精密单点定位(precise point position,PPP)结果,其中采用动力学广域差分改正数,收敛后定位精度可达到15cm;采用运动学广域差分改正数,收敛后定位精度可达45cm。  相似文献   

16.
针对BP (Back Propagation)神经网络模型预测卫星钟差中权值和阈值的最优化问题, 提出了基于遗传算法优化的BP神经网络卫星钟差短期预报模型, 给出了遗传算法优化BP神经网络的基本思想、具体方法和实施步骤. 为验证该优化模型的有效性和可行性, 利用北斗卫星导航系统(BeiDou navigation satellite system, BDS)卫星钟差数据进行钟差预报精度分析, 并将其与灰色模型(GM(1,1))和BP神经网络模型预报的结果比较分析. 结果表明: 该模型在短期钟差预报中具有较好的精度, 优于GM(1,1)模型和BP神经网络模型.  相似文献   

17.
全球导航卫星系统(global navigation satellite system,GNSS)的信号质量评估是卫星导航系统设计和运行过程中的重要环节.在简要介绍导航信号特点的基础上,介绍了基于监测数据的信号稳定性评估方法,最后从伪距原始观测数据、伪距拟合残差、伪距拟合残差标准差3个层面进行了评估,给出了在Matlab环境下评估的具体结果.分析结果进一步证实了该方法的正确性和可行性.该方法有助于保证全球导航卫星系统空间信号的连续性和可靠性.  相似文献   

18.
利用精密星历解算卫星坐标是实现全球定位系统高精度差分定位的首要基础,受限于全球定位系统精密星历的采样时间间隔,为了得到任意时刻的卫星坐标,需要对全球定位系统精密星历数据做内插和外推处理。分析卫星位置随时间变化的规律后,采用广义延拓法对卫星的一段轨道构造以时间为坐标的内插和外推模型,在不引入较大位置误差的同时简化了卫星坐标的计算过程,并与拉格朗日插值法进行对比实验。研究结果表明,利用广义延拓法内插时误差小于5 cm,且在外推30 min内仍然能维持精度,明显优于拉格朗日插值法。  相似文献   

19.
The recent Galileo spacecraft explored Jupiter and its satellite system and provided us with new geodetic data. In order to discuss the dynamical parameters and secular tidal effect of Io, the theory of synchronous satellite is described in detail. Using the new geodetic data of Io, two sets of Io‘s internal structure models are constructed based on the asthenosphere assumption. The liberation parameters α,β,γ and dynamical flattening H are calculated for the models of Io. A comparison of Io with the Moon indicates the they are quite different in many characteristics in spite of the fact that they are approximately equal in mass and size and that they both orbit synchronously.  相似文献   

20.
电离层延迟改正模型综述   总被引:12,自引:0,他引:12  
电离层延迟改正模型通常可以分为广播星历用的预报模型、广域差分用的实时模型、后处理模型3类,不同应用要求需要选择不同的模型。主要比较分析了几种常用的电离层延迟改正模型: 用于广域差分中生成格网模型的三角级数模型、多项式模型、低阶球谐函数模型等都可以获得很好的改正效果,且这3种模型基本上是等价的;电离层延迟谐函数展开模型可以用来分析电离层长时间系列的变化特征;国际电离层参考模型IRI的改正精度一般可以达到60%的效果;而GPS 星历采用的Klobuchar模型的参数设置存在一些不足,对此提出了一些改进措施。  相似文献   

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