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1.
导航电文星历参数对卫星轨道精度的影响 总被引：1，自引：0，他引：1
卫星导航定位的关键是获知导航卫星的精确位置,其轨道精度与导航电文中广播星历参数密切相关。分析了由广播星历参数计算的卫星广播轨道与精密星历确定的真实轨道之间的误差,并将其投影到卫星切向、径向和法向进行仿真研究。比较了民用导航电文（CNAV）和旧民用导航电文（NAV）的星历参数的差异,利用精密星历拟和出对应的广播星历参数,研究其星历参数的变化对卫星轨道精度的影响。分析了GPS不同频点播发的导航电文中星历参数在数据帧内的结构。研究结果表明：GPS卫星广播轨道误差一周内在2到4m内变化,而其在切向、径向和法向的投影值呈现周期性余弦变化,其演变周期与GPS轨道周期近似相等,而选取改进后的17个广播轨道参数表示的星历数据于15个星历参数对比,其轨道拟和误差值改善2～3cm. 相似文献
2.
LEO卫星轨道根数型星历参数与接口设计 总被引：1，自引：1，他引：0
低轨卫星是导航增强系统发展的新兴力量,具有独特优势。广播星历参数是其实现星基增强的重要指标。中轨GPS星历采用16/18参数模型,若直接用于LEO的星历参数拟合,卫星沿迹方向的位置分量拟合误差大,且对小偏心率近圆轨道有潜在的拟合法矩阵病态问题。基于第一类无奇点根数,通过增加或修改轨道沿迹向和径向摄动参数,设计了适用于近圆低轨卫星的16～19参数的5种星历模型。基于300～1500 km高度LEO的拟合试验表明:提出的16/17/18/18~*/19参数星历,URE最大值分别优于10/6/4/5/2.5 cm。最后,根据拟合参数的变化范围,对5个星历模型进行了接口设计。在数据截断对URE的影响为毫米量级要求下,总比特位分别为329/343/376/379/396,其中16/17参数星历模型比GPS16参数模型减少了29/15个,18/18~*/19参数星历模型比GPS18参数星历模型减少了64/61/41个。 相似文献
3.
GPS长距离和多测段定位中广播星历的改进方法 总被引：2，自引：0，他引：2
本文分析了广播星历误差对ＧＰＳ长基线和多测段定位结果的影响，由此提出了旨在减弱卫星轨道误差对于相对定位精度影响的一种简便而又实用的方法，即先按卫星运动的力学模型建立状态方程，其初始状态向量由某组广播星历得出，由每组广播星历建立观测方程，由数值积分得出的参考轨道由广播星历ｔｏｅ时刻的位置和速度观测值的最小二乘平差所得的改正后的轨道，不仅可消除各组广播星历间的不一致性，而且其精度也高于任何一组广播星历 相似文献
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5.
Computer simulation experiment is very important in the phase of project design, the availability of simulated result highly depends on the scheme of error simulation. Time series observations are normally correlated. This paper first discusses the formula of correlated error propagation, then derives the formula of simulating time series correlated errors. This formula is then used to simulate correlated ephemerides errors of CHAMP, then the ephemerides are used to recover the gravity vector at satellite altitude with finite differential formula. The formulae derived in this paper are verified with the difference between the recovered gravity vectors and the `true values' which are directly computed with the same gravity model as that generating the ephemerides. 相似文献
6.
低轨导航增强卫星的轨道状态型星历参数设计 总被引：1，自引：0，他引：1
导航增强卫星从高轨拓展到低轨,需要设计可靠的低轨道LEO广播星历参数。GLONASS广播星历模型能够利用9个状态参数高精度描述30min内中高轨卫星的摄动运动,但不能直接用于低轨卫星。为了适应LEO的摄动力的短期快变化,设计了基于轨道状态型的21参数广播星历模型。分析了低轨卫星主要摄动力的短期变化规律,选取了二次多项式和基于轨道半周期的三角函数来补偿大气阻力等主要摄动在3个方向上的累计。基于星历拟合试验讨论了拟合参数个数、拟合时段和数据间隔对500~1200km轨道高度的LEO圆轨道的拟合精度影响。试验表明,当拟合时段为20min(约1/5个轨道周期)时,轨道高度大于700km的近圆轨道,拟合用户距离误差(FURE)精度优于0.05m;高度为1000km时,FURE平均精度达到0.03m。 相似文献
7.
无旋转倾角的NAV/CNAV型GEO广播星历拟合 总被引：1，自引：1，他引：0
目前北斗GEO的星历拟合算法和用户卫星位置算法均引进了人为设置的5°倾角旋转,此外,少数星历参数还有超限现象。取消GEO的旋转倾角和抑制参数超限能够统一北斗混合星座的用户算法。基于第一类无奇点根数,分析了无旋转倾角的GEO两步法星历参数拟合算法。讨论了GEO的参数超限原因,提出采用固定1至2个超限参数取值的缩减参数拟合法。北斗GEO卫星在非地影期和地影期的拟合试验表明,拟合成功率和拟合精度能够保证,拟合用户距离误差(URE)的平均值优于3mm;缩减参数拟合法能够抑制特定时段下的参数超限问题,但是拟合URE放大到2cm。 相似文献
8.
Until recently, the Global Positioning System (GPS) was the only operational means of distributing time to an arbitrary number
of users and of synchronizing clocks over large distances with a high degree of precision and accuracy. Over the last few
years it has been shown that similar performance can be achieved using the Russian Global Navigation Satellite System (GLONASS).
GLONASS time transfer between continents was initially hampered by the lack of post-processed precise ephemerides. Results
from the International GLONASS Experiment (IGEX) campaign are now available, however, and this paper reports on the first
use of IGEX precise ephemerides for GLONASS P-code intercontinental time links. The results of GLONASS P-code and GPS C/A-code
time transfer are compared under similar conditions.
Received: 31 January 2000 / Accepted: 10 July 2000 相似文献
9.
Broadcast vs. precise GPS ephemerides: a historical perspective 总被引：6，自引：2，他引：4
The Navstar Global Positioning System (GPS) Operational Control Segment (OCS) generates predicted satellite ephemerides and clock corrections that are broadcast in the navigation message and used by receivers to estimate real-time satellite position and clock corrections for use in navigation solutions. Any errors in these ephemerides will directly impact the accuracy of GPS based positioning. This paper compares the satellite position computed using broadcast ephemeredes with the precise position provided by the International GPS Service for Geodynamics (IGS) Final Orbit solution. Similar comparisons have been undertaken in the past, but for only short periods of time. This paper presents an analysis of the GPS broadcast ephemeris position error on a daily basis over the entire operational lifetime of the GPS system. The comparison was undertaken from 14 November 1993 through to 31 December 2002. The statistics of these errors were also analyzed.Disclaimer: The views expressed in this article are those of the authors and do not reflect the official policy or position of the Royal Australian Air Force, Australian Defense Organization, Australian government, United States Air Force, US Department of Defense, or the US Government. 相似文献
10.
Summary The status of nutation theory in the computation of the Earth Rotation Parameters from the different observational techniques
is reviewed. The impact on the combined solution of the Bureau International de l'Heure is evaluated. In view of the improvement
brought by the IAU 1980 Nutation Theory, its introduction in the BIH publications, without waiting for the adoption by the
astronomical ephemerides (1984 Jan. 1) is decided. 相似文献
11.
利用地球重力场模型计算CHAMP卫星参考轨道 总被引：3，自引：1，他引：3
结合CHAMP卫星观测数据的动力法反演，研究了CHAMP卫星参考轨道的数值方法。分别通过利用40～50阶重力位系数模型计算轨道，并与业已公布的卫星轨道数据进行比较，结果表明，CHAMP(低轨)卫星轨道对重力场低频部分的敏感度较大，考虑低阶(40阶左右)重力场模型计算的卫星参考轨道精度较高。 相似文献
12.
本文介绍了中国GIG’91和Epoch’92二次GPS会战的情况,着重分析了GIG’91和Epoch’92会战数据处理的结果。结果证明,利用1－2星期质量良好的数据（含分布均匀的部分全球跟踪站数据）,解算的未知区域性跟踪站地心坐标的重复性可以达到几个厘米,站间基线分量的重复性可以达到10－8或更好。利用中国国内4个跟踪站的数据,由5天轨道弧解算的卫星星历与全球精密星历之差在1－3米水平,平均差一般小于1米。我们的研究证明,参加GPS国际会战,是迅速提高区域性跟踪站地心坐标精度和建立区域性高精度地心坐标框架的有效途径,利用区域性跟踪站可有效地改进GPS卫星轨道的精度,形成全国范围的大尺度的控制,进一步改进GPS测量的精度。 相似文献
13.
Computation of broadcast ephemerides is a fundamental task in satellite navigation and positioning. The GPS constellation is composed of medium-earth-orbit (MEO) satellites, and therefore can employ a uniform parameter set to produce broadcast ephemerides. However, other navigation satellite systems such as Compass and IRNSS may include a mixture of inclined-geosynchronous-orbit (IGSO), geostationary-earth-orbit (GEO) and MEO satellites, requiring different parameter sets for each type of orbit. We analyze the variational characteristics of satellite ephemerides with respect to orbital elements; then present a method to design an optimal parameter set for broadcast ephemerides, and derive the parameter sets for IGSO, GEO, and MEO satellites. The computational complexities of the user algorithms for the optimal parameter sets are equivalent to that of the standard GPS user algorithm. Simulation and statistical analyses indicate that the optimal parameter set is $ \left\{ {\sqrt {A_{0} } ,e_{0} ,i_{0} ,\Upomega_{0} ,M_{0} ,\omega_{0} ,\dot{\Upomega },\dot{u},\dot{i},C_{\Upomega c3} ,C_{\Upomega s3} ,C_{uc2} ,C_{us2} ,C_{rc2} ,C_{rs2} } \right\} $ for IGSO and GEO satellites, and $ \left\{ {\sqrt {A_{0} } ,e_{0} ,i_{0} ,\Upomega_{0} ,M_{0} ,\omega_{0} ,\dot{\Upomega },\dot{u},\dot{i},C_{uc2} ,C_{us2} ,C_{rc2} ,C_{rs2} ,C_{ic2} ,C_{is2} } \right\} $ for MEO satellites. 相似文献
14.
利用GPS载波相位观测值进行基线测定具有重要意义。本文讨论了基线测定中卫星星历误差对定位结果的影响,提出了基线上轨道改进的定位方法,编制了基线测定的定位软件,并使用高精度基线上的实际观测资料进行了计算。计算结果表明在基线上用轨道改进定位方法是可行的,可以提高定位精度。 相似文献
15.
Different types of GPS clock and orbit data provided by the International GPS Service (IGS) have been used to assess the accuracy
of rapid orbit determination for satellites in low Earth orbit (LEO) using spaceborne GPS measurements. To avoid the need
for reference measurements from ground-based reference receivers, the analysis is based on an undifferenced processing of
GPS code and carrier-phase measurements. Special attention is therefore given to the quality of GPS clock data that directly
affects the resulting orbit determination accuracy. Interpolation of clock data from the available 15 min grid points is identified
as a limiting factor in the use of IGS ultra-rapid ephemerides. Despite this restriction, a 10-cm orbit determination accuracy
can be obtained with these products data as demonstrated for the GRACE-B spacecraft during selected data arcs between 2002
and 2004. This performance may be compared with a 5-cm orbit determination accuracy achievable with IGS rapid and final products
using 5 min clock samples. For improved accuracy, high-rate (30 s) clock solutions are recommended that are presently only
available from individual IGS centers. Likewise, a reduced latency and more frequent updates of IGS ultra-rapid ephemerides
are desirable to meet the requirements of upcoming satellite missions for near real-time and precise orbit determination. 相似文献
16.
Integrated adjustment of CHAMP, GRACE, and GPS data 总被引：16，自引：3，他引：13
Various types of observations, such as space-borne Global positioning system (GPS) code and phase data, accelerometer data, K-band range and range-rate data, and ground-based satellite laser ranging data of the CHAllenging Minisatellite Payload (CHAMP) and GRAvity Climate Experiment (GRACE) satellite missions, are used together with ground-based GPS code and phase data in a rigorous adjustment to eventually solve for the ephemerides of the CHAMP, GRACE, and GPS satellites, geocenter variations, and low-degree gravity field parameters. It turns out that this integrated adjustment considerably improves the accuracy of the ephemerides for the high and low satellites, geocenter variations, and gravity field parameters, compared to the case when the adjustment is carried out stepwise or in individual satellite solutions.Acknowledgments. This study has been supported by the German Ministry of Education and Research through the Geotechnologies Programme grants 03F0333A/CHAMP and 03F0326A/GRACE. 相似文献
17.
基于GPS单频接收机的精密单点定位研究 总被引：1，自引：0，他引：1
介绍了利用单频GPS接收机进行精密单点定位的数学模型及解算方案,并采用选权拟合法得到比较准确的状态参数初值及其方差-协方差,加快了卡尔曼滤波的收敛。算例结果表明,利用精密卫星星历及卫星钟改正数并采用单频观测值,半个小时后的定位精度可达1~2分米的水平。 相似文献
18.
Polynomial interpolation of GPS satellite coordinates 总被引：4，自引：2，他引：4
This article describes an algorithm for polynomial interpolation of GPS satellite coordinates and its implementation in MATLAB.
The algorithm is intended for real-time processing software and computes the position and velocity of GPS satellites from
both broadcast and precise ephemerides. Tests with different orders of polynomials, and with different time spans used for
polynomial fitting, show suitable settings with respect to the required interpolation precision. 相似文献
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导航卫星自主定轨的算法研究及模拟结果 总被引：5，自引：2，他引：5
讨论了利用卫星-卫星间的距离观测值建立导航卫星系统自主定轨的数学方法，并用GPS星座模拟星间观测值，采用滤波算法计算卫星的状态参数。模拟结果表明，在空间测距精度一定的情况下，自主定轨精度能高于GPS广播星历，因而能较精确地维持卫星系统的坐标框架。 相似文献