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1.
Measurements consistency-based Receiver Autonomous Integrity Monitoring (RAIM) is the main technique for monitoring the integrity of global satellite navigation systems at the user-level. Existing RAIM algorithms utilize two tests, in the position domain a test for RAIM availability and in the measurement domain a test for failure detection. These tests involve the computation of three parameters: test statistic, decision threshold, and protection level. The test statistic is based on the actual measurements in the form of the sum of the squared errors (SSE). The decision threshold is chosen on the basis of the statistical characteristics of the SSE including the assumption that the errors are normally distributed. However, in practice residual, error distributions exhibit heavier tails than predicted by the Gaussian model. Therefore, this paper challenges the normality assumption of the residual navigation errors in three ways. First, real data are used to assess its impact on the traditional RAIM algorithm. Second, extreme value theory is applied to the tails, and the generalized extreme value (GEV) distribution is derived to capture residual navigation errors. Third, the performance of the traditional RAIM approach is compared with that employing the GEV distribution. The results demonstrate that the GEV model is a more accurate representation of the distribution of residual navigation errors than the conventional Gaussian model and should be used in the development of integrity monitoring algorithms. 相似文献
2.
Pseudorange-based integrity monitoring, for example receiver autonomous integrity monitoring (RAIM), has been investigated
for many years and is used in various applications such as non-precision approach phase of flight. However, for high-accuracy
applications, carrier phase-based RAIM (CRAIM), an extension of pseudorange-based RAIM (PRAIM) must be used. Existing CRAIM
algorithms are a direct extension of PRAIM in which the carrier phase ambiguities are estimated together with the estimation
of the position solution. The main issues with the existing algorithms are reliability and robustness, which are dominated
by the correctness of the ambiguity resolution, ambiguity validation and error sources such as multipath, cycle slips and
noise correlation. This paper proposes a new carrier phase-based integrity monitoring algorithm for high-accuracy positioning,
using a Kalman filter. The ambiguities are estimated together with other states in the Kalman filter. The double differenced
pseudorange, widelane and carrier phase observations are used as measurements in the Kalman filter. This configuration makes
the positioning solution both robust and reliable. The integrity monitoring is based on a number of test statistics and error
propagation for the determination of the protection levels. The measurement noise and covariance matrices in the Kalman filter
are used to account for the correlation due to differencing of measurements and in the construction of the test statistics.
The coefficient used to project the test statistic to the position domain is derived and the synthesis of correlated noise
errors is used to determine the protection level. Results from four cases based on limited real data injected with simulated
cycle slips show that residual cycle slips have a negative impact on positioning accuracy and that the integrity monitoring
algorithm proposed can be effective in detecting and isolating such occurrences if their effects violate the integrity requirements.
The CRAIM algorithm proposed is suitable for use within Kalman filter-based integrated navigation systems.
相似文献
| Shaojun FengEmail: |
3.
接收机自主完好性监测（RAIM）是卫星导航系统完好性监测的方法之一。一定时空条件下的RAIM可用性,可以通过RAIM空洞直观的反映出来,可以为飞行提供预警;利用不同期GPS、GLONASS实际星座,仿真分析了单星座以及GPS／GLONASS组合星座RAIM可用性,绘制了RAIM空洞图,具有一定的参考价值。 相似文献
4.
接收机自主完好性监测(receiver autonomous integrity monitoring,RAIM)是终端用户高可靠导航定位的保障,低轨卫星的发展为完好性监测带来新的机遇,然而不同低轨星座增强下的终端RAIM性能可能会存在显著差异。基于高轨道倾角(80颗)、中轨道倾角(120颗)和混合轨道倾角(168颗)3种典型的低轨星座,系统评估了低轨卫星增强下的北斗卫星导航系统（BeiDou navigation satellite system,BDS）RAIM可用性及故障检测效果。仿真计算结果表明：对于高纬区域,高轨道倾角增强下的RAIM可用性效果最好,而在中、低纬区域,中轨道倾角星座增强下的RAIM可用性效果最优;在全球范围内,高轨道倾角、中轨道倾角和混合轨道倾角星座增强下非精密进近阶段的RAIM可用性较BDS分别提升30.5%、29.0%和41.0%。由此可知,由不同轨道倾角组成的混合星座可较好地弥补可视卫星在空间覆盖上的缺陷,其全球RAIM可用性增强效果最优,增强下的RAIM可检测到的最小伪距偏差较之前平均减小33.3 m。 相似文献
5.
针对基于最小二乘残差估计的接收机自主完好性监测(RAIM)算法,结合伪距单点定位多采用观测量非等权模型,提出一种观测量非等权模型RAIM可用性算法,对实际计算具有借鉴意义。通过实测数据,分析了等权模型和非等权模型RAIM可用性算法对卫星几何分布的估计情况,验证了观测量非等权模型RAIM可用性算法的可行性。 相似文献
6.
In the Global Positioning System, there is no provision for real-time integrity information within the Standard Positioning Service, by design. However, in safety critical sectors like aviation, stringent integrity performance requirements must be met. This can be achieved using the special augmentation systems or RAIM (Receiver Autonomous Integrity Monitoring) or both. RAIM, the most cost-effective method relies on data consistency, and therefore requires redundant measurements for its operation. An external aid to provide this redundancy can be in the form of an Inertial Navigation system. This should enable continued performance even when no redundant satellite measurements are available. An algorithm presented in previous papers by the authors detects the rate of slowly growing errors. The algorithm was shown to be effective for early detection of slowly growing errors that belong to the class of most difficult to detect errors. Firstly, rate detector is tested for varying faults. Secondly, real data are used to validate the rate detector algorithm. The data are extensively analyzed to ascertain whether it is suitable for integrity and fault diagnostics. A modification to the original rate detector algorithm is suggested by addition of a bias state to the dynamic model. The performance is then compared with the existing techniques and substantial improvement is shown. 相似文献
7.
An Assessment of the RAIM Performance of a Combined Galileo/GPS Navigation System Using the Marginally Detectable Errors (MDE) Algorithm 总被引：1，自引：0，他引：1
W. Y. Ochieng K. F. Sheridan K. Sauer X. Han P. A. Cross S. Lannelongue N. Ammour K. Petit 《GPS Solutions》2002,5(3):42-51
Integrity relates to the trust that can be placed in the correctness of information supplied by a navigation system. It includes
the ability of the navigation system to provide timely warning to users when the system fails to meet its stated accuracy.
Specifically, a navigation system is required to deliver a warning (alarm) when the error in the derived user position solution exceeds an allowable level (alarm limit). This warning must be issued to the user within a given period of time (time-to-alarm) and with a given probability (integrity risk). The two main approaches to monitoring the integrity of satellite navigation systems are Receiver Autonomous Integrity Monitoring
(RAIM), and monitoring based on an independent network of integrity monitoring stations and a dedicated Ground Integrity Channel
(GIC). More recently Satellite Autonomous Integrity Monitoring (SAIM) methods have also been investigated.
This article presents the results of a study to assess the RAIM capability of the Galileo system when used alone and when
combined with the Global Positioning System (GPS). The assessment was based on the Marginally Detectable Error (MDE) algorithm.
The results show a significant improvement in the capability to perform RAIM using a combined Galileo/GPS system compared
to the performance using the Galileo system alone. This study was supported by Alcatel Space and was a contribution to the
Galileo definition studies carried out for the European Community under the GALA project. ? 2002 Wiley Periodicals, Inc. 相似文献
8.
把导航领域、军事领域和导航电子地图中广泛应用的圆概率误差(circular error probable,CEP)引入到HPL(horizontal protection level)的计算中,在最小二乘残差法基础上构建了基于圆概率误差的RAIM(receiver autonomous integrity monitoring)可用性算法。首先计算了在一定误警率、漏警率条件下多颗卫星发生故障时的水平定位偏差和一定置信度下的圆概率误差;然后以GPS导航星座为例,探讨了相关观测下计算HPL的新方法;最后把HPL与水平告警限差(horizontal alert limit,HAL)相比较,得到了基于圆概率误差的RAIM可用性,并通过算例验证了此方法的有效性和可行性。 相似文献
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GNSS接收机自主完备性监测高级算法的有效性验证 总被引：1，自引：0，他引：1
针对RAIM的高级算法———ARAIM,使之应用于对GNSS完备性和生命安全要求更高的领域,基于GNSS实测数据对ARAIM算法下的垂直保护水平、精度、有效监测阈值、连续性风险进行了研究,并对ARA-IM算法下GNSS的可用性进行了评估。结果表明,相对于GPS系统而言,GPS/GLONASS系统下的垂直保护水平、精度、有效监测阈值、连续性风险及可用性完全满足LPV-200阶段的导航性能要求,验证了ARAIM算法在预测垂直保护水平、精度、有效监测阈值、连续性风险方面的有效性。 相似文献
12.
A fast and efficient integrity computation for non-precision approach performance assessment 总被引：1，自引：0，他引：1
The level of safety to be expected from global positioning system (GPS) must be known in order to use it to support safety
critical operations such as air navigation. This is captured by the navigation performance parameter of integrity which includes
the ability of the navigation system to deliver a warning to the user in the event of a significant failure and within a specified
time-to-alert. Given the high percentile requirement associated with integrity, assessment of expected system performance
both in the nominal case and during failure events, requires the application of analytical techniques. This paper identifies
the weaknesses of the current methods for assessing the level of performance to be expected of GPS for non-precision approaches
and proposes ways to address them including a novel application of a mathematical integration technique that greatly reduces
the computational load associated with integrity performance calculations. Results based on computation times show that the
new method reduces computational load by a factor of 500+ with a high accuracy and associated high level of confidence. It
is shown that in some cases, the technique presented is able to improve GPS RAIM availability beyond the gains achieved by
measurement weighting. 相似文献
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鉴于独立分量对异常值具有较强的敏感性,提出了基于独立分量分析(ICA)的伪距多变量时间序列异常值探测算法,并且利用契比雪夫不等式给出了异常值探测的阈值,引入时间序列干预模型估计了潜在故障扰动的大小,根据3σ准则确定出故障星的位置。根据RAIM的实时性要求,采用滑动窗口的思想对上述批处理探测算法进行改造,本文提出了一种卫星多故障在线探测和识别的新算法,并给出了新RAIM算法的实施流程。利用5个iGMAS北斗监测站的民用观测数据对新算法进行验证,试验分析结果表明,新算法对于卫星多故障的实时处理具有较好的效果,且其故障正确探测率优于以往的RANCO方法。 相似文献
15.
In the absence of obstacles, a GPS device is generally able to provide continuous and accurate estimates of position, while in urban scenarios buildings can generate multipath and echo-only phenomena that severely affect the continuity and the accuracy of the provided estimates. Receiver autonomous integrity monitoring (RAIM) techniques are able to reduce the negative consequences of large blunders in urban scenarios, but require both a good redundancy and a low contamination to be effective. In this paper a resampling strategy based on bootstrap is proposed as an alternative to RAIM, in order to estimate accurately position in case of low redundancy and multiple blunders: starting with the pseudorange measurement model, at each epoch the available measurements are bootstrapped—that is random sampled with replacement—and the generated a posteriori empirical distribution is exploited to derive the final position. Compared to standard bootstrap, in this paper the sampling probabilities are not uniform, but vary according to an indicator of the measurement quality. The proposed method has been compared with two different RAIM techniques on a data set collected in critical conditions, resulting in a clear improvement on all considered figures of merit. 相似文献
16.
Dong-Hwan Hwang Sang Heon Oh Sang Jeong Lee Chansik Park Chris Rizos 《GPS Solutions》2005,9(4):294-311
Due to their complementary features of GPS and INS, the GPS/INS integrated navigation system is increasingly being used for
a variety of commercial and military applications. An attitude determination GPS (ADGPS) receiver, with multiple antennas,
can be more effectively integrated with a low-cost IMU since the receiver gives not only position and velocity data but also
attitude data. This paper proposes a low-cost attitude determination GPS/INS integrated navigation system. The proposed navigation
system comprises an ADGPS receiver, a navigation computer unit (NCU), and a low-cost commercial MEMS IMU. The navigation software
includes a fault detection and isolation (FDI) algorithm for integrity. In order to evaluate the performance of the proposed
navigation system, two flight tests have been performed using a small aircraft. The first flight test confirmed the fundamental
operation of the proposed navigation system and the effectiveness of the FDI algorithm. The second flight test evaluated the
performance of the proposed navigation system and demonstrated the benefit of GPS attitude information in a high dynamic environment.
The flight test results show that the proposed ADGPS/INS integrated navigation unit gives reliable navigation performance
even when anomalous GPS data is provided and gives better navigation performance than a conventional GPS/INS unit. 相似文献
17.
介绍了RAIM算法中故障检测及其完好性保证的原理,采用STK仿真得到GPS和Galileo系统的卫星坐标及中国区域内的格网点坐标,结合航空用户对完好性需求,比较了GPS和Galileo系统下、不同类型导航性能需求的RAIM算法的可用性结果,分析了截止高度角、可视卫星数对故障检测可用性的影响。结果表明:当截止高度角越低、可视卫星数越多,故障检测的可用性越高;相同截止高度角条件时,Galileo系统下的RAIM可用性要高于GPS系统;单一的GPS导航系统难以满足垂直引导进近和精密进近等高等级的航空需求。 相似文献
18.
随着空间时间频率基准的精度越来越高,需要与之匹配的空间时频传递技术. 基于载波相位的星地双向时差测量方法可以实现更高的时间频率传递精度,但对于复杂的星地环境,由于航天器飞行动态高,时频传递链路的传输频率高,载波多普勒效应大,更容易出现粗差和周跳. 基于此,研究一种适合高动态环境下的星地双向时差测量系统载波相位周跳探测与修复方法,提出一种适用于三频组合模式的双向周跳探测与修复方法. 该方法联合双频码相 (MW)组合法可以实现不同类型周跳的探测与修复,对于上下行三条微波链路均可探测出周跳的存在并实现毫米级周跳修复精度. 进一步对基于载波相位测量的星地双向时差测量系统的星地时间同步性能进行分析,在经过周跳探测与修复,以及链路时延数据处理,其星地时间同步精度优于0.3×10–12 s. 相似文献
19.
针对GNSS接收机在室内环境中面临的强烈的信号衰减、非视距传播和互相关效应的问题,提出了一种基于粗时段导航和RAIM算法解决A-GNSS室内定位问题的方法,并利用BDS数据验证了该方法的可靠性。结果表明,粗时段导航算法能够提供连续可靠的定位结果,应用于微弱信号环境;基于组合FDE的RAIM算法能够增加定位结果可用率,解决室内卫星信号存在的非视距传播和互相关效应的问题。基于粗时段导航与RAIM算法的A-GNSS定位技术能够应用于室内定位,仿真定位结果水平方向RMS在10 m以内。 相似文献
20.
This paper will describe an enhancement to the GPS double difference carrier phase measurements on a single airborne platform
by smoothing them with inertial measurements while preserving the dynamic bandwidth. This enhancement will reduce the impact
of carrier phase multipath and carrier phase noise on baseline determination between multiple antennas on an aircraft when
in flight. This type of measurement system has numerous applications where platform pointing and relative body motion must
be determined at the mm-level for applications such as sensor stabilization, Synthetic Aperture Radar, long range RADAR (i.e.
angle-of-arrival measurements). Lower noise levels (mm-level and below) enable more performance to the stabilized system such
as increased aperture for longer range, operation at higher frequencies, and more image resolution. The focus of this paper
will be on a technique to provide this enhanced performance for these various applications using the available navigation
systems. Additionally, this type of smoothing can effectively remove the additional noise induced by carrier phase measurement
differencing. The noise level of a double or triple difference can be reduced below that of the raw measurement. A complimentary
synthesized double difference quantity with ultra-low-noise characteristics will be used to smooth the GPS carrier phase double
difference measurements without losing dynamic bandwidth since it follows the airborne dynamics. Flight test data will be
presented to demonstrate the performance improvement in the midst of aircraft dynamics. Results will show that the noise reduction
follows the theoretical prediction. 相似文献