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71.
可编程数字锁相环的研制 总被引:1,自引:0,他引:1
介绍一种可编程数字锁相环。它由单片机和数字锁相环构成。其中锁相环的工作状态和参数由单片机处理和控制。这样能较好地解决稳态误差与稳态建立时间之间的矛盾,基本上实现了在保证稳态误差小的同时,可大幅度地缩短稳态建立时间的目的,使原来的数字锁相环的性能更优。 相似文献
72.
一种研究圆柱度目标函数单谷性的新方法 总被引:1,自引:0,他引:1
提出了一种研究圆柱目标函数单谷性的新方法,圆柱度目标函数单谷性的问题目前研究得还少,而弄清楚圆柱度目标函数是否是单谷函数对于用优化原理正确地计算其极值是非常重要的。 相似文献
73.
介绍一种新的激光准直系统,该系统通过单模光纤建立新的光发射基准,从而有效地抑制了由于激光腔热变形而产生的光束漂移。另外,该系统采用了标量卡尔曼数字滤波器耒降低大气扰动和其他环境因素对测量的影响,在2.5m的测量范围内,系统稳定性可以控制在±1.5μm以下。该系统适用于作为形状误差和运动误差测量时的直线基准。 相似文献
74.
在激光测角干涉仪中,由于角度棱镜安置的方位不同,将导致该仪器角度测量范围的变化。分析了角度棱镜的方向和位置对角度测量范围的影响,比较了不同方案的优劣,并给出了结论。 相似文献
75.
76.
电离层延迟是全球卫星导航系统(GNSS)的主要误差源之一。对于装配GNSS单频接收机的航空器,选择简单有效的Klobuchar广播电离层模型来改正电离层延迟误差,其修正率为50%~60%。针对45°(N)纬度带,提出了更高电离层修正需求。考虑到季节因素对中高纬度地区电离层的显著影响,利用GIMs(Global Ionospheric Maps)分析了昼夜中TEC(Total Electron Content)的峰值和谷值随季节(年积日)的变化,建立了一种适用于45°(N)纬度带的Klobuchar like电离层模型。该模型不增加广播模型系数,新模型的夜间和VTEC高峰时电离层修正率分别达到了82%和80%,表明在穿刺点集中的45°(N)纬度地区使用该模型可以更精确地描述该地区的电离层,帮助航空器实现更高精度的定位。 相似文献
77.
Raul Orus Perez 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2019,63(5):1607-1618
In the last 20?years, and in particular in the last decade, the availability of propagation data for GNSS has increased substantially. In this sense, the ionosphere has been sounded with a large number of receivers that provide an enormous amount of ionospheric data. Moreover, the maturity of the models has also been increased in the same period of time. As an example, IGS has ionospheric maps from GNSS data back to 1998, which would allow for the correlation of these data with other quantities relevant for the user and space weather (such as Solar Flux and Kp). These large datasets would account for almost half a billion points to be analyzed. With the advent and explosion of Big Data algorithms to analyze large databases and find correlations with different kinds of data, and the availability of open source code libraries (for example, the TensorFlow libraries from Google that are used in this paper), the possibility of merging these two worlds has been widely opened. In this paper, a proof of concept for a single frequency correction algorithm based in GNSS GIM vTEC and Fully Connected Neural Networks is provided. Different Neural Network architectures have been tested, including shallow (one hidden layer) and deep (up to five hidden layers) Neural Network models. The error in training data of such models ranges from 50% to 1% depending on the architecture used. Moreover, it is shown that by adjusting a Neural Network with data from 2005 to 2009 but tested with data from 2016 to 2017, Neural Network models could be suitable for the forecast of vTEC for single frequency users. The results indicate that this kind of model can be used in combination with the Galileo Signal-in-Space (SiS) NeQuick G parameters. This combination provides a broadcast model with equivalent performances to NeQuick G and better than GPS ICA for the years 2016 and 2017, showing a 3D position Root Mean Squared (RMS) error of approximately 2?m. 相似文献
78.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2020,65(1):560-571
The precise point positioning (PPP) technique is widely used in time and frequency applications. Because of the real-time service (RTS) project of the International GNSS Service, we can use the PPP technique for real-time clock comparison and monitoring. As a participant in the RTS, the Centre National d’Etudes Spatiales (CNES) implements the PPPWIZARD (Precise Point Positioning with Integer and Zero-difference Ambiguity Resolution Demonstrator) project to validate carrier phase ambiguity resolution. Unlike the Integer-PPP (IPPP) of the CNES, fixing ambiguities in the post-processing mode, the PPPWIZARD operates in the real-time mode, which is also called real-time IPPP (RT-IPPP). This paper focuses on applying the RT-IPPP for real-time clock comparison and monitoring. We review the principle of real-time clock comparison and monitoring, and introduce the methodology of the RT-IPPP technique. The observations of GPS, GLONASS and Galileo were processed for the experiments. Five processing modes were provided in the experiment to analyze the benefits of ambiguity resolution and multi-GNSS. In the clock comparison experiment, the average reduction ratios of standard deviations with respect to the G PPP mode range from 9.7% to 35.0%. In the clock monitoring experiment, G PPP mode can detect clock jumps whose magnitudes are larger than 0.9 ns. The RT-IPPP technique with GRE PPP AR (G) mode allows for the detection of any clock jumps larger than 0.6 ns. For frequency monitoring, G PPP mode allows detection of frequency changes larger than 1.1 × 10−14. When the RT-IPPP technique is applied, monitoring with GRE PPP AR (G) mode can detect frequency changes larger than 6.1 × 10−15. 相似文献
79.
Zhuo Li Tisheng Zhang Farui Qi Hailiang Tang Xiaoji Niu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2019,63(7):2164-2174
Since the signals of global navigation satellite system (GNSS) are blocked frequently in challenging environments, the discontinuous carrier phases seriously affect the application of GNSS precise positioning. To improve the carrier phase continuity, this paper proposes a carrier phase prediction method based on carrier open-loop tracking. In the open-loop tracking mode, the carrier numerically controlled oscillator (NCO) is controlled by the predicted Doppler, but not by the loop filter output. To improve the phase prediction effective time, accurate receiver clock drift estimation is studied in the prediction method. The phase prediction performance is tested on GNSS software receiver. In the phase prediction effective time tests, open-loop processes were set for the tested channel. The test results show that, when some satellite signals are blocked in 15?s, the probability of carrier phase error less than quarter cycles is more than 94%. In the real time kinematic (RTK) positioning tests, some satellite signals are blocked in 10–15?s repeatedly. The test results show that, the carrier phase continuity is basically not affected by the signal interruption, and the RTK can almost keep continuous centimeter-level positioning accuracy without re-fixing the integer ambiguity. 相似文献
80.