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1.
Approximations to composite GPS protection levels for aircraft precision approach and landing 总被引：1，自引：1，他引：0
Persistent pseudorange biases constitute a serious potential integrity problem for differential GPS systems used in aircraft precision approach and landing. Various approaches to solve this problem are documented in the literature, including composite protection levels (PLs) that incorporate an explicit bias term in their mathematical expressions. A statistical characterization for such a PL was previously presented in this journal. Modeling GPS error in the position domain as multivariate normal with nonzero mean resulted in the definition of vertical, horizontal, and radial composite PLs, termed VPLc, HPLc, and RPLc, respectively. In the present effort, approximations to these computationally intensive PLs are presented for possible use in real time. Two of these are shown to be over-bounding approximations to exact quantities VPLc and HPLc. An approximation to RPLc is also presented, as well as a method of quantitative evaluation for each of these composite PLs. Monte-Carlo simulations for a single GPS measurement epoch are then developed to illustrate the exact PLs and their approximations and demonstrate that the approximations to VPLc and HPLc over-bound the exact PLs. The approximation to RPLc is shown to be far simpler computationally than the exact PL, but demonstrating that the approximation is an over-bound is left to future research. This paper makes available to the reader both the methods and the Matlab? simulation code needed to evaluate computationally efficient PL approximations. Thus, it fosters further research into the use of GPS in safety critical applications. 相似文献
2.
提出了一种基于指数平滑法的GPS卫星钟差预报方法。该方法可采用少量数据建模,且计算过程简单、方便,尤其是在缺少相关历史数据或数据变化趋势不明显、不稳定的情况下,用该方法仍可取得较好的效果。通过与GPS卫星钟差预报中常用的二次多项式模型和灰色预测模型的对比分析,结果表明:指数平滑法适用于GPS卫星钟差的中、短期预报,其预报精度可达ns级;在利用小数据量建模的情况下,其预报效果优于二次多项式模型,与灰色模型的预报效果基本相当;该方法还可用于GPS卫星钟差的长期预报,其预报精度可达μs级,与灰色预测模型的精度相当。 相似文献
3.
根据卫星钟固有的特性,即频移、频漂和频漂率以及周期性,提出一种新的拟合方法。新方法首先构造一个合理的钟差模型,该模型包含一个二次多项式和多个周期项。然后利用IGS提供的钟差产品数据,先粗略补充缺失数据,用二次多项式拟合;并对拟合后的残差进行小波分析,作降噪处理;最后通过谱分析,确定其主要的周期项,从而构建出适当的拟合模型,实现精密GPS卫星钟差拟合和预报。多天数据的实验结果表明,采用本文提出的新方法能够有效地对卫星钟差进行拟合和预报,满足不同目的的需求。 相似文献
4.
利用SLR和伪距资料确定导航卫星钟差 总被引：6，自引：0，他引：6
提出了综合利用SLR和GPS伪距资料测定导航卫星钟差的方法,采用2002年10月的SLR和伪距实测数据计算了GPS 35卫星的钟差,并对GPS 35卫星的钟差进行了预报,为了验证计算结果的精度,将本文计算的卫星钟差与IGS精密钟差进行了比较.通过比较分析发现:综合利用SLR和伪距资料测定的导航卫星钟差精度优于3 ns,测定的导航卫星钟差与实际卫星钟差不存在系统差;导航卫星钟差的预报精度与计算卫星钟速的时间跨度有关;可以分离卫星坐标和卫星钟差之间的相互影响,便于对卫星钟差的研究. 相似文献
5.
6.
Jan Douša 《GPS Solutions》2010,14(3):229-239
The impact of precise GPS ephemeris errors on estimated zenith tropospheric delays (ZTD) is studied for applications in meteorology.
First, the status of IGS ultra-rapid orbit prediction is presented and specific problems are outlined. Second, a simplified
analytical solution of the impact of ephemeris errors on estimated ZTDs is presented. Two widely used methods are studied—the
precise point positioning technique (PPP) and the double-difference network approach. A simulation experiment is additionally
conducted for the network approach to assess the capability of ephemeris error compensation by the ambiguities. An example
of marginal requirements for ephemeris accuracy is presented, assuming the compensation by ZTD only and admitting the error
of 1 cm in ZTD. The requirement for the maximum orbit error 1 cm for radial and 8 cm for tangential position components using
PPP approach, versus 217 cm (radial) and 19 cm (tangential) using network solution. Furthermore, an assessment of possible
compensations of ephemeris errors by other estimated parameters was considered. In radial orbit position, an error of a few
meters can be still absorbed by satellite clocks (96%) and phase ambiguities (96%) even for the PPP technique. A tangential
orbit position error up to 16 cm for PPP and 38 cm for network solutions should not bias ZTD by more than 1 cm, but any bigger
error could, in general. The error impact on ZTD in such cases depends on the compensation ability of ambiguities and clocks
(PPP). 相似文献
7.
神经网络在卫星钟差短期预报中的应用研究 总被引：2，自引：0，他引：2
本文针对卫星钟差的特点,提出了基于神经网络的卫星钟差短期预报模型,给出了基于径向基函数(RBF)网络进行卫星钟差预测的基本思想、预测模型和实施步骤,并对比分析了神经网络模型与灰色系统理论模型的区别.为验证本文提出的预报模型的可行性和有效性,利用GPS卫星钟差数据进行钟差预报精度分析,并与灰色系统模型进行对比分析.仿真结... 相似文献
8.
A new model for GPS yaw attitude 总被引：7，自引：4，他引：3
Yoaz E. Bar-Sever 《Journal of Geodesy》1996,70(11):714-723
modeling of the GPS satellite yaw attitude is a key element in high-precision geophysical applications. This fact is illustrated here as a new model for the GPS satellite yaw attitude is introduced. The model constitutes a significant improvement over the previously available model in terms of efficiency, flexibility and portability. The model is described in detail and implementation issues, including the proper estimation strategy, are addressed. The performance of the new model is analyzed and an error budget is presented. Finally, the implementation of the yaw bias on the GPS satellites is reviewed from its inception until it reached a steady state in November, 1995. 相似文献
9.
10.
Impact of GPS differential code bias in dual- and triple-frequency positioning and satellite clock estimation 总被引：1，自引：0，他引：1
The features and differences of various GPS differential code bias (DCB)s are discussed. The application of these biases in dual- and triple-frequency satellite clock estimation is introduced based on this discussion. A method for estimating the satellite clock error from triple-frequency uncombined observations is presented to meet the need of the triple-frequency uncombined precise point positioning (PPP). In order to evaluate the estimated satellite clock error, the performance of these biases in dual- and triple-frequency positioning is studied. Analysis of the inter-frequency clock bias (IFCB), which is a result of constant and time-varying frequency-dependent hardware delays, in ionospheric-free code-based (P1/P5) single point positioning indicates that its influence on the up direction is more pronounced than on the north and east directions. When the IFCB is corrected, the mean improvements are about 29, 35 and 52% for north, east and up directions, respectively. Considering the contribution of code observations to PPP convergence time, the performance of DCB(P1–P2), DCB(P1–P5) and IFCB in GPS triple-frequency PPP convergence is investigated. The results indicate that the DCB correction can accelerate PPP convergence by means of improving the accuracy of the code observation. The performance of these biases in positioning further verifies the correctness of the estimated dual- and triple-frequency satellite clock error. 相似文献
11.
Satellite clock bias estimation for iGPS 总被引：4，自引：0，他引：4
John Pratt Penina Axelrad Kristine M. Larson Bruno Lesage Richard Gerren Nicholas DiOrio 《GPS Solutions》2013,17(3):381-389
The High Integrity GPS program seeks to provide enhanced navigation performance by combining conventional GPS with a communications and ranging broadcast from the Iridium® Communications System. Through clock and message aiding, it would enable existing GPS receivers to acquire and track in more challenging environments. As is the case for standard GPS, accurate and precise timing is key to performance. An approach is presented for estimating the bias of each Iridium satellite clock using satellite-to-ground and satellite-to-satellite measurements. The satellite clock bias estimates are based on a Kalman filter that incorporates code-type observations from the measurements at 10 s intervals. Filter parameters are set based on the expected behavior of the clocks, allowing for discontinuous bias and frequency adjustments due to ground commands. Typical results show the current filter to be accurate to within 200 ns while always meeting the initial system specification of half a microsecond. 相似文献
12.
Due to increased demands on the quality of the results of Global Positioning System (GPS) evaluations, various authors have studied improvements of the stochastic model of GPS carrier-phase observations. These improvements are based on the reasonable assumption that the commonly used stochastic model with independent and homoscedastic (i.e. equal variance) errors is unrealistic. However, this has not been proved rigorously so far. A statistical test procedure based on uncorrelated least–squares residuals, which allows verification of the hypothesis of a heterogeneous variance, is provided. The statistical test procedure is of interest in its own right, and is independent of the practical problem considered. The presented technique is applied to GPS carrier-phase observations. Results show that the variances of the investigated observations are far from homogeneous. It is indicated that the error variances of the presented data increase with decreasing GPS satellite elevation. These results confirm the assumption that the commonly used stochastic model of GPS observations is inadequate and has to be improved. 相似文献
13.
Summary The signals transmitted by Block II satellites of the Global Positioning System (GPS) can be degraded to limit the highest accuracy of the system (10 m or better point positioning) to authorized users. This mode of degraded operation is called Selective Availability (S/A). S/A involves the degradation in the quality of broadcast orbits and satellite clock dithering. We monitored the dithered satellite oscillator and investigated the effect of this clock dithering on high accuracy relative positioning. The effect was studied over short 3-meter and zero-baselines with two GPS receivers. The equivalent S/A effects for baselines ranging from 0 to >10,000 km can be examined with short test baselines if the receiver clocks are deliberately mis-synchronized by a known and varying amount. Our results show that the maximum effect of satellite clock dithering on GPS double difference phase residuals grows as a function of the clock synchronization error according to: S/A
effect
=0.04 cm/msec, and it increases as a function of baseline length like: S/A
effect
=0.014 cm/100 km. These are equations for maximum observed values of post-fit residuals due to S/A. The effect on GPS baselines is likely to be smaller than the 0.14 mm for a baseline separation of 100 km. We therefore conclude, for our limited data set, and for the level of S/A during our tests, that S/A clock dithering has negligible effect on all terrestrial GPS baselines if double difference processing techniques are employed and if the GPS receivers remain synchronized to better than 10 msec. S/A may constitute a problem, however, if accurate point processing is required, or if GPS receivers are not synchronized. We suggest and test two different methods to monitor satellite frequency offsets due to S/A. S/A modulates GPS carrier frequencies in the range of-2 Hz to +2 Hz over time periods of several minutes. The methods used in this paper to measure the satellite clock dither could be applied by the civilian GPS community to continuously monitor S/A clock dithering. The monitored frequencies may aid high accuracy point positioning applications in a postprocessing mode (Malys and Ortiz 1989), and differential GPS with poorly synchronized receivers (Feigl et al. 1991). 相似文献
14.
15.
北斗全球卫星导航系统(简称北斗三号系统,BDS-3)的建设对拓展全球卫星导航系统(global naviga tionsatellitesystem,GNSS)的应用有重要作用,为多星座融合定位、导航和授时提供了重要支持.多系统融合定位给用户提供了更多的导航信息源,也为导航卫星系统完好性和用户自主完好性指标的实现提供了... 相似文献
16.
卫星频间钟差偏差（Inter-Frequency Clock Bias, IFCB）变化特性的分析对其模型化、卫星钟稳定性的评估具有重要的意义。采用北斗(COMPASS) 2012年1月的三频数据,解算了GEO卫星的IFCB并分析了其时序特性。为了削弱粗差对解算结果的影响,采用了抗差估计算法。针对GEO卫星IFCB的特性,提出了GEO卫星IFCB的经验模型。结果表明,二次曲线函数能较好的描述GEO卫星的IFCB,并达到71%以上的改正效果。 相似文献
17.
Statistics of GPS ionospheric scintillation and irregularities over polar regions at solar minimum 总被引：2，自引：1，他引：1
A statistical study of the occurrence characteristic of GPS ionospheric scintillation and irregularity in the polar latitude
is presented. These measurements were made at Ny-Alesund, Svalbard [78.9°N, 11.9°E; 75.8°N corrected geomagnetic latitude
(CGMLat)] and Larsemann Hills, East Antarctica (69.4°S, 76.4°E; 74.6°S CGMLat) during 2007–2008. It is found that the GPS
phase scintillation and irregularity activity mainly takes place in the months 10, 11 and 12 at Ny-Alesund, and in the months
5, 6 at Larsemann Hills. The seasonal pattern of phase scintillation with respect to the station indicates that the GPS phase
scintillation occurrence is a local winter phenomenon, which shows consistent results with past studies of 250 MHz satellite
beacon measurements. The occurrence rates of GPS amplitude scintillation at the two stations are below 1%. A comparison with
the interplanetary magnetic field (IMF) B
y and B
z components shows that the phase scintillation occurrence level is higher during the period from later afternoon to sunset
(16–19 h) at Ny-Alesund, and from sunset to pre-midnight (18–23 h) at Larsemann Hills for negative IMF components. The findings
seem to indicate that the dependence of scintillation and irregularity occurrence on geomagnetic activity appears to be associated
with the magnetic local time (MLT). 相似文献
18.
在实时GPS精密单点定位中,能否快速有效地得到高精度的卫星钟差预报值是影响实时单点定位速度和精度的一个重要因素,由于GPS原子钟的高频率、高敏感和极易受到外界及其本身因素影响的性质使得卫星钟差预报至今都没能得到很好地解决,本文在目前的卫星钟差预报基础上,分别探讨了利用灰色模型理论、线性模型和二次多项式模型等方法,以IGS超快星历中2004年12月7日卫星钟差观测资料预报8日的卫星钟差为例进行卫星钟差预报研究,初步得出如下结论:在利用IGS超快星历的前一天的卫星钟差观测值预报后一天的钟差时,线性模型相对方便有效;而灰色模型只要选取合适的模型指数系数,能得到较高精度;但二次多项式模型预报精度较差。利用线性模型能达到或优于IGS超快星历预报钟差的预报精度。 相似文献
19.
Marek Ziebart Paul Cross Antony Sibthorpe Peter Arrowsmith Washington Ochieng Shaojun Feng Umar Bhatti Peter Niemann 《GPS Solutions》2007,11(4):227-237
The Galileo integrity chain depends on a number of key factors, one of which is contamination of the signal-in-space errors
with residual errors other than imperfect modelling of satellite orbits and clocks. A potential consequence of this is that
the user protection limit is driven not by the errors associated with the imperfect orbit and clock modelling, but by the
distortions induced by noise and bias in the integrity chain. These distortions increase the minimum bias the integrity chain
can guarantee to detect, which is reflected in the user protection limit. A contributor to this distortion is the inaccuracy
associated with the estimation of the offset between the Galileo sensor station (GSS) receiver clocks and the Galileo system
time (GST). This offset is termed the receiver clock synchronization error (CSE). This paper describes the research carried
out to determine both the CSE and its associated error using GPS data as captured with the Galileo System Test Bed Version
1 (GSTB-V1). In the study we simulate open access to a time datum using IGS data. Two methods are compared for determining
CSE and the corresponding uncertainty (noise) across a global network of tracking stations. The single-epoch single-station
method is an ‘averaging’ technique that uses a single epoch of data, and is carried out at individual sensor stations, without
recourse to the data from other stations. The global network solution method is also single epoch based, but uses the inversion
of a linearised model of the global system to solve for the CSE simultaneously at all GSS along with a number of other parameters
that would otherwise be absorbed into the CSE estimate in the averaging technique. To test the effectiveness of various configurations
in the two methods the estimated synchronisation errors across the GSS network (comprising 25 stations) are compared to the
same values as estimated by the International GPS Service (IGS) using a global tracking network of around 150 stations, as
well as precise orbit and satellite clock models determined by a combination of global analysis centres. The results show
that the averaging technique is vulnerable to unmodelled errors in the satellite clock offsets from system time, leading to
receiver CSE errors in the region of 12 ns (3.7 m), this value being largely driven by the satellite CSE errors. The global
network approach is capable of delivering CSE errors at the level of 1.5 ns (46 cm) depending on the number of parameters
in the linearised model. The International GNSS Service (IGS) receiver clock estimates were used as a truth model for comparative
assessment. 相似文献
20.
Improved method for estimating the inter-frequency satellite clock bias of triple-frequency GPS 总被引：1，自引：0，他引：1
Considering the contribution of the hardware biases to the estimated clock errors, an improved method for estimating the satellite inter-frequency clock bias (IFCB) is presented, i.e., the difference in the satellite clock error as computed from ionospheric-free pseudorange and carrier phase observations using L1/L2 and P1/P2 versus L1/L5 and P1/P5. The IFCB is composed of a constant and a variable part. The constant part is the inter-frequency hardware bias (IFHB). It contains the satellite and receiver hardware delays and can be expressed as a function of the DCBs [DCB (P1 ? P2) and DCB (P1 ? P5)]. When a reference satellite is selected, the satellite IFHB can be computed but is biased by a reference satellite IFHB. This bias will not affect the utilization of IFCB in positioning since it can be absorbed by the receiver clock error. Triple-frequency observations of 30 IGS stations between June 1, 2013, and May 31, 2014, were processed to show the variations of the IFHB. The IFHB values show a long-term variation with time. When a linear and a fourth-order harmonic function are used to model the estimated IFCB, which contains contributions of the hardware delays and clock errors, the results show that 89 % of the IFCB can be corrected given the current five triple-frequency GPS satellites with the averaged fitting RMS of 1.35 cm. Five days of data are processed to test the estimated satellite clock errors using the strategy presented. The residuals of P1/P5 and L1/L5 have a STD of <0.27 m and 0.97 cm, respectively. In addition, most predicted satellite IFCBs reach an accuracy of centimeter level and its mean accuracy of 5 days is better than 7 cm. 相似文献