共查询到18条相似文献，搜索用时 93 毫秒
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GPS单点测速的误差分析及精度评价 总被引：6，自引：0，他引：6
首先从理论和实测数据模拟两方面分析了SA取消后各类误差源对GPS测速的影响,推导并计算了GPS单点测速可能达到的精度水平。然后用静态数据模拟动态测速试验和实测动态数据测速与同步高精度惯导测速的动态试验进行验证。结果表明,采用载波相位导出的多普勒观测值使用静态数据模拟动态测速,其精度可以达到mm/s级;用接收机输出的多普勒观测值进行测速时,其精度为cm/s级。在动态测速试验中,GPS单点测速方法（即多普勒观测值测速与导出多普勒观测值测速）间的符合精度达到cm/s级,与高精度的惯导测速结果的符合精度为dm/s级,而且和运动载体的动态条件（如加速度和加速度变化率的大小）具有很强的相关性。 相似文献
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GPS单点测速的误差分析及精度评伤 总被引：1，自引：0，他引：1
首先从理论和实测数据模拟两方面分析了sA取消后各类误差源对GPS测速的影响,推导并计算了GPs单点测速可能达到的精度水平.然后用静态数据模拟动态测速试验和实测动态数据测速与同步高精度惯导测速的动态试验进行验证.结果表明,采用栽波相位导出的多普勒观测值使用静态数据模拟动态测速,其精度可以达到mm/s级;用接收机输出的多普勒观测值进行测速时,其精度为cm/s级.在动态测速试验中,GPS单点测速方法(即多普勒观测值测速与导出多普勒观测值测速)间的符合精度达到cm/s级,与高精度的惯导测速结果的符合精度为dm/s级,而且和运动载体的动态条件(如加速度和加速度变化率的大小)具有很强的相关性. 相似文献
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为了满足地质灾害实时高精度监测应用需求，对常规全球卫星导航系统(GNSS)载波相位差分测速事后处理软件进行改进，增加了实时数据流接收和实时解码国际海运事业无线电技术委员会(RTCM)的功能，实现了真正的GNSS载波相位差分测速.利用静态站和振动台模拟正弦波振动实验的GNSS数据，评估改进后GNSS实时测速程序的精度.静态模拟动态的测速精度误差均方根(RMS)优于5 mm/s；振动台动态实验解算结果与振动台输出真值的互差RMS为10.4 mm/s.说明本实验的实时GNSS测速程序在静态实时测速条件下的测速精度可达到mm/s级，在实时动态条件下测速精度仍能达到cm/s级. 相似文献
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为分析单、双频手机在单点定位和动态导航中的差异,本文对单、双频手机观测卫星数、信噪比、静态/动态定位中原始观测值/卡尔曼滤波值进行了对比和分析。试验结果表明,在静态无遮挡的试验条件下,小米MI8双频手机原始观测值较OPPO Reno单频手机定位误差均值减小了1.70 m且能观测到更多的卫星数,进行卡尔曼滤波处理后,单频手机较双频手机而言精度提升更多,两者最终精度相当。而在动态有遮挡的试验条件下,双频较单频定位误差均值减小了5.24 m,进行卡尔曼滤波处理后,两者精度均有明显改善,双频相对单频误差均值减小了0.87 m。 相似文献
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速度是载体运动状态的重要表征,高精度定速能力是BDS-3系统高性能服务的重要体现。针对传统单站历元间相位差分模型易受误差积累与观测环境影响等问题,本文提出了顾及载体航向约束的单站BDS-3相位测速模型。首先,在传统BDS-3历元间相位差分方程矢量分解的基础上,构建载体位移增量微分表达式,联合非差模型与微分方程综合估计载体速度;其次,利用载体水平面内位移矢量与航向角之间的相关性,建立顾及航向角约束的N与E方向位移参数约束条件;最后,综合3组独立的函数方程进行载体速度分量逐历元解算。通过静态与动态试验表明,静态条件下,BDS-3相位不同方向均可实现mm/s的测速精度,相较于传统历元间差分模型,E与N方向分别提升了62.9%和87.5%,且有效避免了水平方向测速误差的积累效应,但U方向由于缺少约束导致精度提升不显著。动态条件下,BDS-3相位测速在直线运动状态水平面内可获得mm/s级的测速精度,且E与N方向较传统历元间差分模型分别提升了35.2%和21.8%,而转向状态E、N、U方向测速精度分别为2.81、2.03和1.91 cm/s,较传统模型分别提升了41.2%、45.9%和56.2%。... 相似文献
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GPS定位以及测速误差中包含有卫星星历误差、电离层、对流层延迟以及多路径效应等多种误差,对GPS的测速精度有着十分重要的影响,减小其误差的一种重要的方法即为卡尔曼滤波。由于GPS测速难以确定动态噪声和观测噪声,因此,标准卡尔曼滤波往往不能时时满足假设条件,而致发散。采取自适应的滤波方法对其进行改进并进行了比较,取得了较好的结果。 相似文献
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Error sources which decrease the accuracy of GPS in absolute velocity determination have been changed since SA was turned off. Firstly, quantities of all kinds of error sources that influence velocity determination are analyzed. The potential accuracy of GPS absolute velocity determination is derived from both theory and field GPS data simulation. After that, two tests were carried out to evaluate the performance of GPS absolute velocity determination in the case of a static and an airborne GPS receiver and INS （Inertial Navigation System） instrument in kinematic mode. In static mode, the receiver velocity has been estimated to be several mm/s with the carrier-phase derived Doppler measurements, and several cm/s with the receiver generated Doppler measurements. In kinematic mode, GPS absolute velocity estimates are compared with the synchronized measurements from the high accuracy INS. The root mean square statistics of the velocity discrepancies between GPS and INS come up to dm/s. Moreover, it has a strong correlation with the acceleration or jerk of the aircraft. 相似文献
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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
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多路径效应与测站观测环境相关,无法利用差分的方式消除或削弱,是GPS精密数据处理时的主要误差源。为此,本文提出了一种利用半天球格网点模型削弱测站多路径误差影响的新方法MHGM(multi-point hemispherical grid model)。该方法对以测站为球心的半天球进行格网点划分,通过格网点的参数化描述,实现测站处多路径误差建模,可适用于现有各类GPS数据处理的软硬件设备和观测环境。本文算例的测试结果表明,采用新方法建模后双差观测值残差的RMS均值改善率平均在73.9%左右,较传统恒星日滤波方法的改善效果平均可提升26.9%,对于静态观测数据,按实时动态相对定位处理模式可获得平面精度约1.7 mm,高程精度约3.0 mm的定位结果。此外,MHGM模型还可进一步用于对测站周边可能存在的多路径误差源进行方位评估,对从物理意义上消除多路径误差源的影响给出一定的指导性意见。 相似文献
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GPS多普勒频移测量速度模型与误差分析 总被引：10，自引：0，他引：10
利用GPS多普勒频移观测量可以获得高精度的速度测量结果。文中先给出GPS载波相位观测方程，在此基础上，详细推导了GPS多普勒频移测量载体速度的数学模型。然后在相对测量模式下，讨论各种误差对速度的影响。 相似文献
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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
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ZHANGXiaohong LIUJingnan 《地球空间信息科学学报》2004,7(3):218-224
The error sources related to the laser rangefinder, GPS and INS are analyzed in details. Several coordinates systems used in airborne laser scanning are set up, and then the basic formula of system is given.This paper emphasizes on discussing the kinematic offset correction between GPS antenna phase center and laser fired point. And kinematic time delay influence on laser footprint position, the ranging errors, positioning errors, attitude errors and integration errors of the system are also explored. Finally, the result shows that thekinematic time delay can be neglected as compared with other error sources. The accuracy of the coordinates is not only influenced by the amplitude of the error, but also controlled by the operation parameters such as flight height, scanning angle amplitude and attitude magnitude of the platform. 相似文献
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The error sources related to the laser rangefinder, GPS and INS are analyzed in details. Several coordinates systems used in airborne laser scanning are set up, and then the basic formula of system is given. This paper emphasizes on discussing the kinematic offset correction between GPS antenna phase center and laser fired point. And kinematic time delay influence on laser footprint position, the ranging errors, positioning errors, attitude errors and integration errors of the system are also explored. Finally, the result shows that the kinematic time delay can be neglected as compared with other error sources. The accuracy of the coordinates is not only influenced by the amplitude of the error, but also controlled by the operation parameters such as flight height, scanning angle amplitude and attitude magnitude of the platform. 相似文献