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天线观测墩及基岩的热膨胀效应会造成GNSS基准站坐标时间序列高程方向的非线性变化。本文提出了一种计算热膨胀效应导致的基准站垂向位移的改进方法:首先利用基岩热膨胀模型和基准站地表温度数据,分别计算热膨胀效应对基准站天线观测墩和基岩的影响量;其次,利用最小二乘拟合方法,同时估计模型中周期项的周期、振幅、相位等信息,而已有方法仅估计振幅与相位信息;最后,基于改进的模型,分析了基准站垂向位移的周期性特征变化。本文利用该方法分析了有代表性的9个IGS基准站的数据。结果表明:基岩热膨胀和天线观测墩热效应能造成测站垂直方向位移变化;在分析的基准站中,最大影响分别可达0.57mm和1.85mm;热膨胀效应造成的GNSS基准站垂直方向位移时间序列具有周年和半周年周期特性,分别可以解释测站U方向坐标时间序列季节性变化的11.2%和3.3%,影响大小随测站纬度的增加而增加,且半周年影响明显小于周年影响;同时,部分测站发现了其他小周期的影响(约51d)。此外,基于该方法,选取了全球107个IGS站,计算了热膨胀造成的各测站垂向位移周年振幅及其相位,结果显示周年振幅最大可达3.3mm,其大小和测站纬度具有比较明显的相关性。 相似文献
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通过精密单点定位的方法获取了区域CORS网各基准站的坐标时间序列,并利用最大似然估计法和频谱分析法对其32个基准站坐标时间序列的周期特征进行了分析,获取了各基准站年周期、半年周期的振幅和相位值,以及各基准站的周期功率谱图。结果表明:GNSS基准站坐标时间序列不仅存在线性变化,还存在周期性变化,其中以U方向表征最为明显,与双差定位获得的坐标时间序列周期特性分析结果一致,说明以精密单点定位获取的GNSS基准站坐标时间序列是可靠的,可以用来分析基准站的变化特征。 相似文献
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为了全面分析我国大陆及其周边GNSS连续站噪声的空间分布规律,该文基于陆态网络260个GNSS连续站和周边区域10个IGS站的观测数据,利用GAMIT/GLOBK软件进行解算,得到各站的坐标值及其N、E、U 3分量误差值,制定筛选标准,依据该标准剔除质量差的测站,剔除异常值;利用Matlab软件,按照东向(E分量)、北向(N分量)、垂向(U分量)3个方向进行拟合,并提取各测站单日解的最大误差值出现的年积日,绘制其在我国大陆的空间分布图,得到中国大陆GNSS连续站最大单日误差值的时空分布特性图。发现大部分GNSS连续站单日最大误差值集中在夏季(7月居多)并分析了原因。 相似文献
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CORS站高程非线性速度场估计方法 总被引：1，自引：0，他引：1
针对以固定周期项的线性拟合模型建立CORS站垂向速度场运动模型的方法,该文设计非线性最小二乘周期拟合算法以线性LS模型的周期项和振幅等作为非线性模型的初值,迭代求解CORS站非线性高程速度场模型的各周期项参数。以Kunm站近12年的高程时间序列为例,近似的年、半年、两年周期等的频率分别为0.999 87、2.018 4、0.500 185,振幅分别为0.17、0.002、0.23cm,非线性速度场模型拟合后的残差中误差由1.34mm降低为1.25mm。实验结果表明,非线性速度场拟合的周期项并不是固定精确的年、半年等,拟合模型的精度有所提高。 相似文献
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针对时间序列混有的高频信息会影响地心运动规律分析的问题，采用网平移法对IGS提供的GNSS周解进行解算，得到2007-2017年地心运动时间序列，对其进行分解重构，剔除高频项，并利用重构时序对地心运动规律作进一步分析探讨。结果表明：本文解算的地心运动在Tx、Ty和Tz方向的精度均为毫米级。EMD方法重构的时序保留了原序列的基本信息，且抑制了高频项的影响，提高了周期贡献率，3个方向的贡献率分别提高了12.3%、16.7%及6.3%。通过分析重构后的时序发现，周年项振幅为各周期对应振幅的最大值，分别为2.32、1.89和2.07 mm；Ty和Tz方向长期变化趋势较Tx更为明显，分别为0.13和-0.27 mm/a；半年项较小，且在Tx和Ty方向上具有时变性。此外，还发现了一些其他较小的年际变化。 相似文献
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随着我国CORS基准站的投入使用,获得了大量高精度连续观测数据,这些数据被广泛应用到测绘行业、航天、航空和军事等许多行业的领域中,因此,对高程时间序列分析有着极其重要的意义。本文先采用Pan Ta方法剔除异常值,然后基于混沌动力学系统,采用Lyapunov指数Wolf方法检验与Lyapunov指数谱矩阵估计对时间序列进行平稳性分析;采用约束实现CAFFT算法生成替代时间序列与Lyapunov指数p-范数检验时间序列非线性。通过分析可知,北京房山站高程时间序列为非线性、非稳态时间序列,观测系统为部分确定性机制低阶混沌动力系统,所以在对该高程时间序列进行拟合、谱估计和周期拟合等数据处理前,必须对数据进行数据相空间重构。 相似文献
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GNSS algebraic structures 总被引：4，自引：3，他引：1
The first objective of this paper is to show that some basic concepts used in global navigation satellite systems (GNSS) are
similar to those introduced in Fourier synthesis for handling some phase calibration problems. In experimental astronomy,
the latter are at the heart of what is called ‘phase closure imaging.’ In both cases, the analysis of the related structures
appeals to the algebraic graph theory and the algebraic number theory. For example, the estimable functions of carrier-phase
ambiguities, which were introduced in GNSS to correct some rank defects of the undifferenced equations, prove to be ‘closure-phase
ambiguities:’ the so-called ‘closure-delay’ (CD) ambiguities. The notion of closure delay thus generalizes that of double
difference (DD). The other estimable functional variables involved in the phase and code undifferenced equations are the receiver
and satellite pseudo-clock biases. A related application, which corresponds to the second objective of this paper, concerns
the definition of the clock information to be broadcasted to the network users for their precise point positioning (PPP).
It is shown that this positioning can be achieved by simply having access to the satellite pseudo-clock biases. For simplicity,
the study is restricted to relatively small networks. Concerning the phase for example, these biases then include five components:
a frequency-dependent satellite-clock error, a tropospheric satellite delay, an ionospheric satellite delay, an initial satellite
phase, and an integer satellite ambiguity. The form of the PPP equations to be solved by the network user is then similar
to that of the traditional PPP equations. As soon as the CD ambiguities are fixed and validated, an operation which can be
performed in real time via appropriate decorrelation techniques, estimates of these float biases can be immediately obtained.
No other ambiguity is to be fixed. The satellite pseudo-clock biases can thus be obtained in real time. This is not the case
for the satellite-clock biases. The third objective of this paper is to make the link between the CD approach and the GNSS
methods based on the notion of double difference. In particular, it is shown that the information provided by a maximum set
of independent DDs may not reach that of a complete set of CDs. The corresponding defect is analyzed. One of the main results
of the corresponding analysis concerns the DD–CD relationship. In particular, it is shown that the DD ambiguities, once they
have been fixed and validated, can be used as input data in the ‘undifferenced CD equations.’ The corresponding algebraic
operations are described. The satellite pseudo-clock biases can therefore be also obtained via particular methods in which
the notion of double differencing is involved. 相似文献
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Dae Hee Won Eunsung Lee Moonbeom Heo Sangkyung Sung Jiyun Lee Young Jae Lee 《GPS Solutions》2014,18(2):177-187
In urban canyons, buildings and other structures often block the line of sight of visible Global Navigation Satellite System (GNSS) satellites, which makes it difficult to obtain four or more satellites to provide a three-dimensional navigation solution. Previous studies on this operational environment have been conducted based on the assumption that GNSS is not available. However, a limited number of satellites can be used with other sensor measurements, although the number is insufficient to derive a navigation solution. The limited number of GNSS measurements can be integrated with vision-based navigation to correct navigation errors. We propose an integrated navigation system that improves the performance of vision-based navigation by integrating the limited GNSS measurements. An integrated model was designed to apply the GNSS range and range rate to vision-based navigation. The possibility of improved navigation performance was evaluated during an observability analysis based on available satellites. According to the observability analysis, each additional satellite decreased the number of unobservable states by one, while vision-based navigation always has three unobservable states. A computer simulation was conducted to verify the improvement in the navigation performance by analyzing the estimated position, which depended on the number of available satellites; additionally, an experimental test was conducted. The results showed that limited GNSS measurements can improve the positioning performance. Thus, our proposed method is expected to improve the positioning performance in urban canyons. 相似文献
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Sergey S. Pospelov Andrey L. Botchkovski Peter A. Krauss Stefan Berberich 《GPS Solutions》2000,4(1):48-55
Software Global Navigation Satellite Systems (GNSS) receivers are those that implement signal correlation processing not in
hardware, but in their software. The main problem for the development of real-time software (SW) multichannel GNSS receivers
is the tremendous amount of calculations to perform signal correlation.
The article reviews recent developments of SW GNSS receivers. The emphasis is made on the computationally effective correlation
processing algorithms and the optimization of processing allocation to the receiver's hardware (HW) and SW.
An architecture is suggested that implements the PRN signals despreading in a special HW preprocessor while all the other
correlation processing functions are still kept in SW. The combination of the most time-consuming processing in HW, and all
signal structure-dependent processing in SW, enables unique flexibility of sophisticated GNSS receiver design based on inexpensive
digital signal processors. ? 2000 John Wiley & Sons, Inc. 相似文献
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全球卫星导航系统（GNSS）目前得到了十分广泛的应用,但是GNSS信号到达地面的功率很低,同时民用信号的格式是公开的,因此极易受到各种无意和人为故意的干扰,会对GNSS定位和授时的精度造成影响．查找和消除干扰源十分重要,目前通用的干扰源查找手段是采用测向设备实现干扰源的交叉定位,但在不知道GNSS干扰源的大致位置时,采用测向设备查找干扰源将耗费很长的时间．如果能够通过提取一些通用接收机的输出量实现干扰源的粗定位,就可以为测向定位提供初始参考位置和大概的查找范围．本文利用几乎所有的通用接收机都能输出的位置信息实现干扰源的粗定位,随着GNSS接收机逼近干扰源,会造成接收机位置信息的丢失,随着GNSS接收机远离干扰源,接收机又会重新获取位置信息,本文利用一定区域内众多受干扰的接收机的位置信息丢失点和位置信息重捕获点来实现干扰源的粗定位．通过仿真验证,分析了该技术的定位误差,仿真结果表明,该方法能够实现GNSS干扰源的粗定位,为进一步准确查找干扰源提供位置参考． 相似文献
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摘要：地面运动物体、航空与航天飞行器的跟踪量中，GNSS被广泛用于运动轨道的实时跟踪、定位，行两运动体的防撞、对接，地面测控网站的定位及统一时等方面。动态测量的关键技术主要包括：快速捕获解算，零相位天线技术，RAIM技术，超冗余组合接收术，载波相位共同跟踪技术，分集合成抗多径干扰技等。 相似文献
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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