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Strong equatorial scintillation is often characterized by simultaneous fast phase changes and deep amplitude fading. The combined effect poses a challenge for GNSS receiver carrier tracking performance. One of the consequences of the strong scintillation is increased navigation message data bit decoding error. Understanding the rate of the data bit decoding error under equatorial scintillation is essential for high accuracy and high integrity applications. We present the statistical relationship between the data bit decoding error occurrences and the intensity of amplitude scintillation based on the processing of intermediate frequency GPS scintillation data collected on Ascension Island in March 2013. A third-order phase lock loop (PLL) is implemented to process the data and to access the data bit error typically expected in conventional receivers. A Kalman filter-based PLL is also used to process the same data to demonstrate that the data bit decoding error can be reduced through advanced carrier tracking designs. 相似文献
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理想情况下,数字锁相环(DPLL)的环路参数可以通过直接计算输入原子钟与压控振荡器(VCO)的相位噪声功率谱交点来确定. 但该方法不能考虑到锁相环(PLL)其他模块的噪声,这会导致输出性能恶化. 针对这一问题,文中从PLL模型出发,基于PLL环路传递函数和幂律谱模型,提出PLL模块噪声的等效方法. 该方法将PLL各模块噪声分别等效到输入和VCO的相位噪声上,使得PLL的噪声传递模型只含有等效输入噪声和等效VCO噪声. 然后可以直接计算两者相位噪声交点并设置合理的环路参数. 通过该方法确定的环路参数可以充分结合输入原子钟信号和VCO信号的相位噪声和频率稳定度特性,弥补了直接计算交点法不能考虑模块噪声的缺点. 实验表明:文中方法所选择的环路参数能使得输出信号具备良好的稳定度,可以为应用于净化原子钟信号的数字锁相装置环路参数的确定提供理论指导. 相似文献
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Methodology for comparing two carrier phase tracking techniques 总被引：1，自引：0，他引：1
The carrier phase tracking loop is the primary focus of the current work. In particular, two carrier phase tracking techniques
are compared, the standard phase tracking loop, i.e., the phase lock loop (PLL), and the extended Kalman filter (EKF) tracking
loop. In order to compare these two different techniques and taking into consideration the different models adopted in each,
it is important to bring them to one common ground. In order to accomplish this, the equivalent PLL for a given EKF has to
be determined in terms of steady-state response to both thermal noise and signal dynamics. A novel method for experimentally
calculating the equivalent bandwidth of the EKF is presented and used to evaluate the performance of the equivalent PLL. Results
are shown for both the L1 and L5 signals. Even though the two loops are designed to track equivalent dynamics and to have
equivalent carrier phase standard deviations, the EKF outperforms the equivalent PLL in terms of both the transient response
and sensitivity. 相似文献
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结合星载寄生式干涉合成孔径雷达(InSAR)的工作原理及高稳定频率源的工作特性,给出了时间和频率同步误差模型。基于该误差模型,分析了时间和频率同步误差对干涉相位的影响,首次推导了同步误差导致的信号去相关。基于星载寄生式InSAR系统的空间几何关系和图像信号模型,详细分析了热噪声、模糊、量化噪声、基线、方位向、配准误差及体散射等去相关效应,给出了考虑上述全部去相关因素时系统的相对测高精度,并仿真分析了以Envisat为主星的寄生式InSAR系统在ASAR雷达7个不同波位下的相对测高性能。理论分析和仿真结果表明,在合理选择轨道和雷达参数的前提下,系统可以达到很好的测高精度。 相似文献
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平台颤振是影响高分辨率卫星影像几何和辐射质量的关键因素。为提高从影像反演平台颤振特性的可行性和可信度,本文提出基于局部频率分析相位相关的智能化视差法颤振探测方法。通过结合结构影像表达和相位相关,并充分利用影像的局部和全局相位信息,减少了辐射变化和噪声等干扰因素对亚像素偏移值估计的影响,同时融入视差法颤振探测框架,保证精确稳健的密集匹配,从而实现高效的平台颤振精密探测。通过采用实际辐射变化数据集的算法对比及采用资源三号卫星影像的颤振探测试验验证了本文方法的有效性。结果表明,局部频率分析相位相关算法在辐射差异和噪声等情况下效果优于其他主流相位相关算法,匹配精度达到0.05个像素,本文颤振探测方法有效估计了资源三号卫星的颤振信息。 相似文献
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A reduced inertial measurement unit (IMU) consisting of only one vertical gyro and two horizontal accelerometers or three orthogonal accelerometers can be used in land vehicle navigation systems to reduce volume and cost. In this paper, a reduced IMU is integrated with a Global Positioning System (GPS) receiver whose phase lock loops (PLLs) are aided with the Doppler shift from the integrated system. This approach is called tight integration with loop aiding (TLA). With Doppler aiding, the noise bandwidth of the PLL loop filters can be narrowed more than in the GPS-only case, which results in improved noise suppression within the receiver. In this paper, first the formulae to calculate the PLL noise bandwidth in a TLA GPS/reduced IMU are derived and used to design an adaptive PLL loop filter. Using a series of vehicle tests, results show that the noise bandwidth calculation formulae are valid and the adaptive loop filter can improve the performance of the TLA GPS/reduced IMU in both navigation performance and PLL tracking ability. 相似文献
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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
9.
为了满足高动态用户及强干扰条件下的应用需求,提出了一种基于卫星信号矢量跟踪的SINS/GPS深组合导航方法,设计了基于FPGA硬件平台的实施方案。利用组合卡尔曼滤波器反馈回路取代了传统接收机中独立、并行的跟踪环路,能够同时完成所有可视卫星信号的跟踪和导航信息处理;通过矢量跟踪算法对所有可视卫星信号进行集中处理,能够增强跟踪通道对信号载噪比变化的适应能力,从而提高接收机在强干扰或信号中断条件下的跟踪性能;根据SINS导航参数和星历信息推测GPS伪码相位和多普勒频移等参数,用以辅助卫星信号的捕获和跟踪,能够大大缩短接收机的搜索捕获时间,并增强接收机在高动态条件下的跟踪性能。基于矢量跟踪的深组合方法不仅在GPS信号短暂中断期间,能够保证系统的导航精度和可靠性,而且在强干扰环境中能够维持较好的伪码相位和载波频率跟踪性能。 相似文献
10.
导航信号经过电子密度不均匀的电离层时,信号的幅度和相位会产生快速随机起伏,即为电离层闪烁。电离层闪烁对接收机信号捕获跟踪以及解调定位都有一定的影响,本文采用理论和仿真的方法分析了电离层闪烁对I,Q支路以及跟踪环路的影响。结果表明:相位闪烁对信号I,Q支路均有影响,幅度闪烁对I支路的影响比较大,在相位闪烁比较强或者幅度闪烁比较强的区域,信号更难跟踪处理。弱闪烁时锁相环(PLL)的跟踪门限约29 dBHz,延迟锁定环路(DLL)的跟踪门限约为20.2 dBHz,强闪烁时PLL跟踪门限约为32 dBHz,DLL的跟踪门限约为22 dBHz。相比而言,载波跟踪环路更加脆弱。同时得到,闪烁越强,载波发生周跳的概率越大,载噪比越高,抗闪烁能力越强。 相似文献
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为满足组合导航系统在高动态环境下的性能要求,设计基于矢量跟踪的GNSS／SINS相干深组合导航方法。利用矢量跟踪环路将所有可视卫星的跟踪和导航解算融为一体,增强通道间的辅助;高动态对载波跟踪影响更大,在通道预滤波中将码环载波环分别用独立的滤波器处理,组合滤波中采用通道间差分降低滤波状态维数,提高计算效率。引入惯导的加速度辅助本地信号参数预测,较精确地测量卫星视线方向的加速度,减小接收机在高动态时段的剩余动态,提高本地信号参数的预测精度。基于矢量跟踪软件接收机搭建相干深组合仿真系统,实验表明该方法在高动态等环境下能提高信号跟踪性能,改善系统的精度、可靠性。 相似文献
12.
The timing error between global navigation satellite system (GNSS) and inertial navigation system (INS) processes limits the integration performance in GNSS/INS integrated systems. In a deeply coupled system, this timing error affects not only the integrated navigation solution, but also the GNSS signal tracking. We propose a time-domain model of INS-aided second-order phase-locked loops (PLLs) in consideration of the INS aiding delay, and analyze the effect of INS aiding delay on the tracking errors in details. In addition, an integrated hardware deeply coupled system platform was developed to verify the impact of time delay on INS-aided PLLs. Simulation and field vehicles testing results demonstrate that the tracking error of the INS-aided PLL caused by aiding delay increases with the lengthening of the delay time, the compression of the bandwidth, and the increase in the acceleration. Testing results verify the proposed model. 相似文献
13.
Use of the L2C signal for inversions of GPS radio occultation data in the neutral atmosphere 总被引：1，自引：0，他引：1
S. V. Sokolovskiy W. S. Schreiner Z. Zeng D. C. Hunt Y.-H. Kuo T. K. Meehan T. W. Stecheson A. J. Mannucci C. O. Ao 《GPS Solutions》2014,18(3):405-416
Results from processing FORMOSAT-3/COSMIC radio occultations (RO) with the new GPS L2C signal acquired both in phase locked loop (PLL) and open loop (OL) modes are presented. Analysis of L2P, L2C, and L1CA signals acquired in PLL mode shows that in the presence of strong ionospheric scintillation not only L2P tracking, but also L1CA tracking often fails, while L2C tracking is most stable. The use of L2C improves current RO processing in the neutral atmosphere mainly by increasing the number of processed occultations (due to significant reduction in the number of L2 tracking failures) and marginally by a reduction in noise in statistics. The latter is due to the combination of reduced L2C noise (compared to L2P) and increased L1CA noise in those occultations where L2P would have failed. This result suggests application of OL tracking for L1CA and L2C signals throughout an entire occultation to optimally acquire RO data. Two methods of concurrent processing of L1CA and L2C RO signals are considered. Based on testing of individual occultations, these methods allow: (1) reduction in uncertainty of bending angles retrieved by wave optics in the lower troposphere and (2) reduction in small-scale residual errors of the ionospheric correction in the stratosphere. 相似文献
14.
Carrier phase multipath error characterization and reduction in single aircraft relative positioning
This paper describes GPS carrier phase (CP) multipath characterization and error reduction techniques and their application
in single aircraft relative positioning. In particular, the single aircraft relative positioning scenario has applications
for high-accuracy multi-sensor stabilization where CP multipath is a major error source that limits system performance. We
will briefly review the requisite multipath theory and discuss models for quantifying the error characteristics. Field-test
data will be used to validate the multipath models considering the underlying assumptions. A basic geometric reflection point
theory will be presented to demonstrate the physical environmental sensitivity of CP multipath to parameters such as surface
flatness and antenna height. Several different quantities will be described as multipath indicators for time-domain detection
and will be compared with a frequency-domain technique. A new multipath detection approach will be introduced that is suitable
to track multipath from time-varying reflection/diffraction points. Finally, the narrow-lane antenna baseline processing technique
will be presented as a real-time approach to mitigate CP noise and multipath errors that is well suited for a very short baseline
single aircraft high accuracy relative positioning system. Field-test results and analysis will be used to illustrate the
key concepts in this paper and to help characterize the total navigation system performance. 相似文献
15.
Metop-GRAS in-orbit instrument performance 总被引：2，自引：1，他引：1
The GRAS instrument on the Metop-A satellite provides more than 600 radio occultation measurement profiles per day. The instrument
is characterized by its wide antenna coverage, high signal-to-noise ratio and an ultra-stable clock reference. The conventional
dual-frequency tracking of GPS signals is under dynamic atmosphere conditions complemented by open loop tracking with sampling
of the signal at a 1 kHz rate, providing an unprecedented view of the signal spectral environment. This paper presents the
instrument performance as derived from analysis of in-orbit measurement data. We show that the noise figure is low enough
to enable mapping of external radio noise variations over the earth’s surface. An error propagation model is presented to
relate instrument characteristics to bending angle performance. This model is also used to illustrate the relation between
filter bandwidth, resolution and measurement noise. The Doppler model, guiding open loop measurements, is found to be accurate
to better than 20 Hz with a possibility for improvement to 10 Hz. The high performance at low altitudes enables the presence
of surface reflections at the −20-dB level to be identified in more than 50% of the occultations. The potential performance
improvements for next generation receivers are discussed. 相似文献
16.
We analyze results from using a temperature-sensing MEMS oscillator as frequency source for the front end of a software-based GNSS receiver. Results show that although MEMS oscillators are highly sensitive to temperature, GNSS receivers can still make use of them even without any form of temperature information or compensation. Nevertheless, using a temperature sensor in close proximity to the resonator can significantly decrease acquisition time and improve tracking performance if the temperature measurements are properly filtered to remove noise. In this case, no negative effect on the measured carrier-to-noise density ratio was detected, and phase-locked tracking of strong signals was possible over a temperature range of ?40 to +85 °C. 相似文献
17.
针对目前DEM（Digital Elevation Model, DEM）数字地形分析的精度评价多数不考虑DEM误差的空间自相关性或仅仅采用经验的自相关性模型问题,本文从DEM插值入手,从理论上推导了插值条件下格网DEM邻域窗口内坡度噪声误差的空间自相关性模型以及坡度精度模型,并选取典型的插值方法和坡度差分算法,从实验角度分析了在顾及和不顾及空间自相关性两种情况下的格网DEM坡度计算模型的噪声精度,实验结果表明：坡度精度受DEM噪声误差的空间自相关性影响较大,并与DEM插值方法和坡度计算模型中的差分算法有关。 相似文献
18.
时荣 《测绘与空间地理信息》2015,(8):175-177
多路径误差分析是北斗卫星导航系统性能评估的一项重要内容。本文给出了一种新的计算3频多路径误差的方法,该方法只需对B1和B2载波相位观测值进行处理就能得到3个频率的伪距多路径误差。利用MGEX跟踪站的数据计算了BDS的多路径误差,从GPS和BDS多路径误差比较以及纬度、轨道和频率因素分析了BDS多路径误差的特性,结果表明,BDS多路径误差小于0．5 m,符合质量检查要求,其性能优于GPS卫星系统。 相似文献
19.
本文研究了一种提高恒温晶振长期稳定性的方法,以GPS/BDS接收机输出的秒脉冲信号为参考信号,校正补偿恒温晶振的频率偏移,在不破坏晶振短期稳定性的前提下,获得更好的长期稳定性. 采用中位值平均滤波和卡尔曼滤波消除相位差的跳变和随机抖动,使用带死区的增量式PID算法控制晶振频率,使其和GPS/BDS接收机输出的秒脉冲信号同步. 测试结果表明:驯服后的晶振和铯钟的钟差峰-峰值不超过47 ns,100 s采样Allan方差为6.22×10?11,10 000 s采样的Allan方差约为1.02×10?12. 证明该驯服方法可以使晶振的长期稳定性得到有效提升,是一种可靠有效的驯服方法. 相似文献
20.
双星敏感器在轨相对热变形分析及修正 总被引：2，自引：0，他引：2
为了获取高质量的对地观测遥感图像,除了有效载荷成像的高分辨率外,还需要卫星平台姿态具有高精度。在双星敏联合姿态确定时,星敏感器之间的相对热变形会对姿态确定带来不利影响,需对热变形误差进行辨识与修正。通过对某遥感卫星在轨遥测数据进行分析,建立了星敏感器在轨结构热变形模型,并对星敏感器热变形进行了在轨修正。采用辨识得到的傅里叶级数的热变形模型参数,对星敏热变形进行在轨修正后,提高了星敏感器的测量精度,减小了星敏感器之间的热变形误差对姿态确定精度的影响,对得到高质量的对地观测遥感图像具有很大的工程应用价值。 相似文献