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1.
Ambiguity validation with combined ratio test and ellipsoidal integer aperture estimator 总被引：4，自引：3，他引：1
Shengyue Ji Wu Chen Xiaoli Ding Yongqi Chen Chunmei Zhao Congwei Hu 《Journal of Geodesy》2010,84(10):597-604
To ensure reliable ambiguity resolution, ambiguity validation is an indispensable step. It has been a challenge for many years
and is far from being resolved. Over the past years, various ambiguity validation methods have been proposed, such as F-ratio test, R-ratio test, difference test, projector test, ellipsoidal integer aperture (EIA) estimator and penalized integer aperture
(PIA) estimator. In this paper, through analysis and testing, we find that, when the aperture region of EIA is not allowed
to be overlapped, the efficiency of ambiguity resolution with EIA is low and it is not applicable to fast static positioning
or real-time kinematic (RTK) applications. Then EIA with overlapped aperture regions is recommended and the resulted fail-rate
becomes upper bound of the actual one. After that, it is suggested that combined use of overlapped EIA and R-ratio test can increase the reliability of ambiguity resolution. Finally, numerical tests are carried out based on practical
buoy data and simulated Galileo data. 相似文献
2.
介绍了病态模型参数估计方法,并将其应用于GPS快速动态定位整周模糊度的解算,实现了模糊度初值的快速准确求解。 相似文献
3.
提出部分模糊度固定的加权电离层模型提高大范围全球卫星导航系统(GNSS)航空定位的精度、可靠性及连续性．该方法的主要思路包括:自适应调整大气扰动等误差影响以实现短基线与长基线两类解算模式之间的灵活切换;施加虚拟电离层观测约束信息,提高基线动态定位的浮点解精度;采用部分模糊度固定方法有效挖掘若干模糊度参数的整周约束．试验表明,提出的方法可提高模糊固定效率与定位精度,克服传统方法有效观测信息利用率不足、定位精度较差、可靠性不高以及连续性较差的问题．实验结果表明,部分模糊度固定算法可在2 min内固定95％以上宽巷模糊度解算与80％以上窄巷模糊度,约20 min后可固定所有模糊度． 相似文献
4.
Global navigation satellite system (GNSS)-based attitude determination has been widely used in the navigation fields. The reliability of attitude determination is indispensable for safety-critical applications. Since the multi-antenna-based attitude determination uses ultra-short baseline carrier phase double differential processing, the incorrect ambiguity resolution and the excessive measurement error are two main factors affecting the reliability of attitude determination. Since the ambiguity correctness validation cannot guarantee the reliability of the attitude solution, therefore an integrity monitoring method is proposed for the attitude determination in the measurement domain. The proposed integrity monitoring method constructs double test statistics to satisfy the requirements of integrity risk and continuity risk, simultaneously. Furthermore, the attitude alarm limit has been derived from the required navigation performance as the threshold to test the availability of attitude determination. The performance of the proposed method is tested by conducting the static and kinematic experiments, respectively. The static results have shown that the proposed integrity monitoring method is able to monitor the ambiguity fault and the excessive measurement noise. The real-world kinematic data have indicated that the proposed method can reduce the maximum attitude error by about 2.3°, when compared with the standalone ratio-test method. 相似文献
5.
Penalized GNSS Ambiguity Resolution 总被引：1，自引：1，他引：1
P. J. G. Teunissen 《Journal of Geodesy》2004,78(4-5):235-244
Global Navigation Satellite System (GNSS) carrier phase ambiguity resolution is the process of resolving the carrier phase ambiguities as integers. It is the key to fast and high precision GNSS positioning and it applies to a great variety of GNSS models which are currently in use in navigation, surveying, geodesy and geophysics. A new principle of carrier phase ambiguity resolution is introduced. The idea is to give the user the possibility to assign penalties to the possible outcomes of the ambiguity resolution process: a high penalty for an incorrect integer outcome, a low penalty for a correct integer outcome and a medium penalty for the real valued float solution. As a result of the penalty assignment, each ambiguity resolution process has its own overall penalty. Using this penalty as the objective function which needs to be minimized, it is shown which ambiguity mapping has the smallest possible penalty. The theory presented is formulated using the class of integer aperture estimators as a framework. This class of estimators was introduced elsewhere as a larger class than the class of integer estimators. Integer aperture estimators, being of a hybrid nature, can have integer outcomes as well as non-integer outcomes. The minimal penalty ambiguity estimator is an example of an integer aperture estimator. The computational steps involved for determining the outcome of the minimal penalty estimator are given. The additional complexity in comparison with current practice is minor, since the optimal integer estimator still plays a major role in the solution of the minimal penalty ambiguity estimator. 相似文献
6.
针对北斗卫星类型间偏差（ISTB）导致载波相位差分高精度定位（RTK）的整周模糊度无法固定问题，本文提出了改进ISTB快速改正方法，在观测量层面仅利用1组不同卫星类型的载波相位差分观测量即可实现ISTB估计与改正，实际应用中较传统方法更具普适性与简易性。该方法的测试结果表明，ISTB值由NH码调制不同引起，不同频点的ISTB值具有不一致性；此外，有无改正ISTB的北斗RTK性能对比反映了ISTB会严重降低整周模糊度固定与RTK定位性能。由此可知，本文方法能够保障现阶段北斗接收机更新换代过程中北斗RTK的高精度与高可靠性能。 相似文献
7.
8.
P. J. G. Teunissen 《Journal of Geodesy》2001,75(7-8):399-407
Carrier phase ambiguity resolution is the key to fast and high-precision GNSS (Global Navigation Satellite System) kinematic
positioning. Critical in the application of ambiguity resolution is the quality of the computed integer ambiguities. Unsuccessful
ambiguity resolution, when passed unnoticed, will too often lead to unacceptable errors in the positioning results. Very high
success rates are therefore required for ambiguity resolution to be reliable. Biases which are unaccounted for will lower
the success rate and thus increase the chance of unsuccessful ambiguity resolution. The performance of integer ambiguity estimation
in the presence of such biases is studied. Particular attention is given to integer rounding, integer bootstrapping and integer
least squares. Lower and upper bounds, as well as an exact and easy-to-compute formula for the bias-affected success rate,
are presented. These results will enable the evaluation of the bias robustness of ambiguity resolution.
Received: 28 September 2000 / Accepted: 29 March 2001 相似文献
9.
首先提出了浮点变换完全去相关法,该方法能够在单历元动态确定整周模糊度。研究了基于载波相位测量的完好性监测方法。利用最小二乘残差构造统计检验量,对整周模糊度进行检测。分析了定位误差保护限与卫星构型、漏警概率的关系。实测数据表明,整周模糊度在单历元动态求解的成功率为100%,增加1颗卫星将使垂直定位误差保护限减少约0.2 m,统计检验量检测周跳的正确率为100%。 相似文献
10.
In order to achieve a precise positioning solution from GPS, the carrier-phase measurements with correctly resolved integer ambiguities must be used. Based on the integration of GPS with pseudolites and Inertial Navigation Systems (INS), this paper proposes an effective procedure for single-frequency carrier-phase integer ambiguity resolution. With the inclusion of pseudolites and INS measurements, the proposed procedure can speed up the ambiguity resolution process and increase the reliability of the resolved ambiguities. In addition, a recently developed ambiguity validation test, and a stochastic modelling scheme (based on-line covariance matrix estimation) are adapted to enhance the quality of ambiguity resolution. The results of simulation studies and field experiments indicate that the proposed procedure indeed improves the performance of single-frequency ambiguity resolution in terms of both reliability and time-to-fix-ambiguity. 相似文献
11.
在传统的GPS单历元动态定位参数估计中,由于先验约束信息较少,模糊度求解和定位性能往往较低。据此,研究了多普勒测速在GPS单历元动态定位中的应用,提出了一种附有GPS多普勒测速信息约束的坐标更新方法,即利用移动载体先验坐标和多普勒测速信息预测当前历元坐标。考虑到该方法进行坐标更新的精度较高和传统单点定位坐标更新的稳健性较强等特点,在此基础上给出了相应的单历元整周模糊度参数求解策略,进一步提高了该方法的定位性能。试验结果表明,所提出的算法相对于传统的无速度信息坐标约束的GPS单历元动态定位算法,其模糊度浮点解精度、模糊度固定率和平均定位精度均有了进一步提高,尤其是在观测卫星数较少、卫星几何结构较差的情况下更为明显。 相似文献
12.
整数相位钟法精密单点定位模糊度固定模型及效果分析 总被引：1，自引：1，他引：0
精密单点定位(PPP)模糊度固定方法有3种:星间单差法、整数相位钟法和钟差解耦法,但目前仅法国CNES公开发布用于整数相位钟法PPP模糊度固定的产品,因此研究基于整数相位钟法的用户端PPP模糊度固定模型很有必要.本文分析了整数相位钟法PPP模糊度固定模型,着重指出该模型与传统浮点解PPP模型的区别;提出一种顾及质量控制的逐级模糊度固定策略用于具体实施PPP模糊度固定.大量动态PPP解算试验表明:与浮点解PPP相比,固定解PPP具有更快的收敛速度且定位精度和稳定性更好. 相似文献
13.
Yanming Feng 《Journal of Geodesy》2008,82(12):847-862
This paper presents a general modeling strategy for ambiguity resolution (AR) and position estimation (PE) using three or
more phase-based ranging signals from a global navigation satellite system (GNSS). The proposed strategy will identify three
best “virtual” signals to allow for more reliable AR under certain observational conditions characterized by ionospheric and
tropospheric delay variability, level of phase noise and orbit accuracy. The selected virtual signals suffer from minimal
or relatively low ionospheric effects, and thus are known as ionosphere-reduced virtual signals. As a result, the ionospheric parameters in the geometry-based observational models can be eliminated for
long baselines, typically those of length tens to hundreds of kilometres. The proposed modeling comprises three major steps.
Step 1 is the geometry-free determination of the extra-widelane (EWL) formed between the two closest L-band carrier measurements,
directly from the two corresponding code measurements. Step 2 forms the second EWL signal and resolves the integer ambiguity
with a geometry-based estimator alone or together with the first EWL. This is followed by a procedure to correct for the first-order
ionospheric delay using the two ambiguity-fixed widelane (WL) signals derived from the integer-fixed EWL signals. Step 3 finds
an independent narrow-lane (NL) signal, which is used together with a refined WL to resolve NL ambiguity with geometry-based
integer estimation and search algorithms. As a result, the above two AR processes performed with WL/NL and EWL/WL signals
respectively, either in sequence or in parallel, can support real time kinematic (RTK) positioning over baselines of tens
to hundreds of kilometres, thus enabling centimetre-to-decimentre positioning at the local, regional and even global scales
in the future. 相似文献
14.
组合码和相位观测值在线解双差模糊度的算法 总被引：4，自引：0，他引：4
如何在线精确地求解整周模糊度,是ＧＰＳ高精度动态相对定位的关键问题。在线解算取决于很多因素：基线长度、数据处理方法、接收机的性能（如双频还是单频）以及抗ＡＳ和ＳＡ的能力等。现代双频ＧＰＳ接收机能获得载波相位和Ｌ１、Ｌ２频道上的精度伪距观测值,组合这４个观测值可进行单历元整周模糊度解算。文中对组合码和相位观测值在线解整周度的算法进行了试验和分析,得出了很有实用意义的结合。 相似文献
15.
An optimality property of the integer least-squares estimator 总被引：36，自引：15，他引：21
P. J. G. Teunissen 《Journal of Geodesy》1999,73(11):587-593
A probabilistic justification is given for using the integer least-squares (LS) estimator. The class of admissible integer
estimators is introduced and classical adjustment theory is extended by proving that the integer LS estimator is best in the
sense of maximizing the probability of correct integer estimation. For global positioning system ambiguity resolution, this
implies that the success rate of any other integer estimator of the carrier phase ambiguities will be smaller than or at the
most equal to the ambiguity success rate of the integer LS estimator. The success rates of any one of these estimators may
therefore be used to provide lower bounds for the LS success rate. This is particularly useful in case of the bootstrapped
estimator.
Received: 11 January 1999 / Accepted: 9 July 1999 相似文献
16.
Nobuaki Kubo 《GPS Solutions》2009,13(4):271-280
Instantaneous real-time kinematic (RTK) techniques are one approach to achieving real-time high-accuracy positioning. The
object of this paper is to show the advantage of adding velocity information to instantaneous RTK positioning. In this paper,
velocity from Doppler frequency measurements is used to help resolve integer ambiguities in the LAMBDA method. In urban areas,
pseudorange measurements can suffer from significant errors due to strong multipath, despite the use of advanced multipath-mitigation
techniques. However, Doppler frequency measurements do not deteriorate as much as pseudoranges, because the multipath error
on Doppler frequency measurements is only in the range of several centimeters. Our proposed method has been tested by both
static and moving users in sub-urban environments. Single-epoch ambiguity fixing performance was improved compared to conventional
ambiguity resolution without velocity information. 相似文献
17.
18.
Reliable ambiguity resolution (AR) is essential to real-time kinematic (RTK) positioning and its applications, since incorrect ambiguity fixing can lead to largely biased positioning solutions. A partial ambiguity fixing technique is developed to improve the reliability of AR, involving partial ambiguity decorrelation (PAD) and partial ambiguity resolution (PAR). Decorrelation transformation could substantially amplify the biases in the phase measurements. The purpose of PAD is to find the optimum trade-off between decorrelation and worst-case bias amplification. The concept of PAR refers to the case where only a subset of the ambiguities can be fixed correctly to their integers in the integer least squares (ILS) estimation system at high success rates. As a result, RTK solutions can be derived from these integer-fixed phase measurements. This is meaningful provided that the number of reliably resolved phase measurements is sufficiently large for least-square estimation of RTK solutions as well. Considering the GPS constellation alone, partially fixed measurements are often insufficient for positioning. The AR reliability is usually characterised by the AR success rate. In this contribution, an AR validation decision matrix is firstly introduced to understand the impact of success rate. Moreover the AR risk probability is included into a more complete evaluation of the AR reliability. We use 16 ambiguity variance–covariance matrices with different levels of success rate to analyse the relation between success rate and AR risk probability. Next, the paper examines during the PAD process, how a bias in one measurement is propagated and amplified onto many others, leading to more than one wrong integer and to affect the success probability. Furthermore, the paper proposes a partial ambiguity fixing procedure with a predefined success rate criterion and ratio test in the ambiguity validation process. In this paper, the Galileo constellation data is tested with simulated observations. Numerical results from our experiment clearly demonstrate that only when the computed success rate is very high, the AR validation can provide decisions about the correctness of AR which are close to real world, with both low AR risk and false alarm probabilities. The results also indicate that the PAR procedure can automatically chose adequate number of ambiguities to fix at given high-success rate from the multiple constellations instead of fixing all the ambiguities. This is a benefit that multiple GNSS constellations can offer. 相似文献
19.
整数相位钟法是精密单点定位（PPP）中应用最广泛的模糊度固定方法之一。利用整数相位钟法进行频率传递的稳定度优于传统PPP，但该方法的钟差计算结果包含系统性偏差，影响时间传递精度。本文介绍了整数相位钟法基本原理，分析了钟差计算结果所包含的系统性偏差成因，提出一种基于星间单差模糊度固定与原子钟精化模型的改进整数相位钟法，并检验改进整数相位钟法的模糊度固定性能与时频传递性能。试验结果表明，改进算法能够有效消除该系统性偏差，利用改进整数相位钟法进行时间传递精度能够达到0.1~0.2 ns，频率传递稳定度达到1.1×10-15/d。 相似文献
20.
精密单点定位中的模糊度不具有整数特性,如何将其准确求解一直是当前研究的热点。且在定位初始阶段,需要经过长时间观测才能使定位精度收敛到厘米、分米级。为解决上述两个问题,可引入惯性导航系统（INS）输出的短时间内高精度的导航信息,以用于辅助模糊度浮点解快速准确地解算。文中分别介绍了直接利用位置信息代入和构建虚拟观测量的两种最小二乘方法,以及这两种方法下INS导航信息精度与模糊度浮点解精度之间的关系。仿真结果表明:惯性信息的辅助作用能够有效地在定位初始阶段提高模糊度解算的效率和精度、缩短收敛时间、改善定位精度。 相似文献