首页 | 本学科首页   官方微博 | 高级检索  
相似文献
 共查询到20条相似文献,搜索用时 62 毫秒
1.
从CMMB(中国移动多媒体广播)体系结构入手,研究了CMMB信号抗多径性能。以信号中有、无循环前缀(CP)为例给出了抗多径性能的详细推导,通过Matlab 7.1对该系统在典型动态多径信道情况下的性能进行了仿真。结果表明:该系统有很强的抗多径能力,在信噪比为30dB时接收CMMB信号与接收普通OFDM(正交频分复用)信号相比,误码率有2个量级的改善,有利于提高导航定位的精度。  相似文献   

2.
调相白噪声背景中高稳频率源参数的估计是一个应用广泛的信号处理问题 ,给出了利用平方拟合估计频率源参数的方法 ,它是最小平方误差意义下的估计 ,并根据模拟的数据对这种方法作了验证。  相似文献   

3.
对遇险目标搜索救援的支持是GALILEO全球卫星导航系统的一项重要民用服务.文章介绍了GALILEO搜索救援子系统(SAR)定位的基本原理.在GALILEO SAR中测量量为时间信号与频率信号,文章详细地给出了两种测量信号的定位方法.基于多传感器信息融合技术,对搜索救援系统中不同测量信号进行综合状态估计.在仿真计算中,采用带噪声的模拟测量数据进行定位,数值计算的结果显示基于多传感器数据融合方法的综合状态估计是可靠的.  相似文献   

4.
研究了利用时域相关法和频域相位加权法,仿真生成具有小数比特时延的实信号,通过数值试验验证了两种方法的一致性和正确性,并且对量化和积分的影响做了分析。最后对射电源信号和双目标探测器信号进行仿真,并通过软件处理机处理得到结果。未来可为VLBI相关处理机的处理精度估计、各类噪声分析及未来多目标试验创造必要条件。  相似文献   

5.
根据北斗二代导航系统扩频信号结构及其性质,研究和仿真了B1频点I支路导航信号的捕获算法,设计了滑动相关器来实现相关,并使用匹配滤波法剥离导航电文上调制的Neumann-Hoffman码。最后对捕获结果进行了误差分析。该算法对接收信号的载波多普勒频移和初始码相位进行粗估计,为导航数据的解调、用户接收机的定位创造了必要条件。  相似文献   

6.
基于小波变换的脉冲星弱信号的去噪方法研究   总被引:1,自引:0,他引:1  
利用小波变换去除噪声的基本原理和方法及消色散方法对毫秒脉冲星极弱信号进行了提取,并对噪声进行了最佳阈值选取实验研究,实现了脉冲星弱信号消色散积累后的检测和抑噪.并研究了软硬阈值估计子等不同阈值消噪技术,进而对PSR 0437-4715信号采用不同方法去噪后的结果进行了分析比较,认为在最大分解层数J=5时对脉冲星信号处理有普适意义.研究结果认为基于小波变换的消噪方法是一种提高信噪比、展示噪声和突变信号的优越方法.  相似文献   

7.
分析了射频前端带宽与BOC信号自相关函数的关系,研究了射频前端带宽和早迟码间距对S曲线的影响。在规范的TOA误差估计模型框架下,采用非相干延时码跟踪锁定环,推导出非相干延时锁定环理论计算的码跟踪误差与射频前端带宽、早迟码间距、载噪比、积分时间和码环路带宽之间的关系表达式,从而定量地分析了非相干延时锁定环的码跟踪误差。最后对BPSK-R信号和BOC(10,5)信号的码跟踪性能做了比较,比较表明,BOC(10,5)信号的码跟踪性能优于传统的BPSK-R信号,在相同的码跟踪精度条件下,BOC(10,5)比10.23 MHz BPSK-R信号所需要的载噪比约低7 dB,比1.023 MHz BPSK-R信号低15 dB左右。  相似文献   

8.
一种基于MUSIC算法的天地波识别方法   总被引:1,自引:0,他引:1  
基于我国BPL长波脉冲信号的特征,利用MUSIC(多信号分类)算法对BPL天、地波延迟进行估计,实现天、地波识别。对传统谱估计IFFT(快速傅里叶逆变换)算法和现代谱估计MUSIC算法进行了仿真和比较,结果表明,这两种方法在较低信噪比条件下可有效分离天、地波,且识别误差都能控制在±5μs内,但MUSIC算法比IFFT算法具有更高的精度和分辨率。  相似文献   

9.
提出了一种基于特征向量算法来估计Loran-C接收机天波延迟的信号处理新技术,为设计具有自适应调节最佳采样点的Loran-C接收机打下良好的基础.建立了基于频谱相除技术的信号模型,简要介绍了特征向量的谱估计算法.研究了此算法估计天波延迟的准确性,并与IFFT技术作了对比.仿真结果显示.特征向量算法比IFFT具有更高的分辨率和尖锐的波峰.最后,通过实测数据的实验验证了这些结论.  相似文献   

10.
罗兰—C导航系统的精度取决于其传播信号的地波部分的高稳定性。这一系统的有效工作范围受到地波信号传播距离和远距离处天波信号干扰的限制。本文叙述了一种测定天波特性的技术,以便估计天波对导航过程的影响,从而改进或扩大罗兰—C系统的导航范围。到目前为止所取得的资料表明:有可能工作在地波脉冲较迟一些的点上,以得到较高的信噪比;并且也有可能以低一些的精度用天波本身导航。文中还提出了进一步研究的工作。  相似文献   

11.
Solar System Research - Finding and studying possible collisions of asteroids approaching the Earth requires a significant amount of computation. This paper describes the R0 program created to...  相似文献   

12.
13.
14.
15.
Many asteroids with a semimajor axis close to that of Mars have been discovered in the last several years. Potentially some of these could be in 1:1 resonance with Mars, much as are the classic Trojan asteroids with Jupiter, and its lesser-known horseshoe companions with Earth. In the 1990s, two Trojan companions of Mars, 5261 Eureka and 1998 VF31, were discovered, librating about the L5 Lagrange point, 60° behind Mars in its orbit. Although several other potential Mars Trojans have been identified, our orbital calculations show only one other known asteroid, 1999 UJ7, to be a Trojan, associated with the L4 Lagrange point, 60° ahead of Mars in its orbit. We further find that asteroid 36017 (1999 ND43) is a horseshoe librator, alternating with periods of Trojan motion. This asteroid makes repeated close approaches to Earth and has a chaotic orbit whose behavior can be confidently predicted for less than 3000 years. We identify two objects, 2001 HW15 and 2000 TG2, within the resonant region capable of undergoing what we designate “circulation transition”, in which objects can pass between circulation outside the orbit of Mars and circulation inside it, or vice versa. The eccentricity of the orbit of Mars appears to play an important role in circulation transition and in horseshoe motion. Based on the orbits and on spectroscopic data, the Trojan asteroids of Mars may be primordial bodies, while some co-orbital bodies may be in a temporary state of motion.  相似文献   

16.
In the text-books of astronomy, sections generally related to the Moon deal with the orbital elements of the Earth-Moon system such asa, e, i, , and the time of perigee passage. While the MEAN of the first of the three elements do not vary, mean longitude of the ascending node-mean longitude of the lunar perigee and the time of perigee passage undergoes secular as well as periodic changes due predominantly to the action of the Sun's gravitational attraction. While to a certain degree, explanations related to the calculation of the lunar orbit parameters are given, not a single graphical representation of these short- or long-periodic changes are presented. We allow the number of data related to these periodic changes must cover a large span of time; and if regression of the line of nodes or advances of the line of apses are to be graphically seen, data covering 18.61 and 8.85 yr, respectively, are needed. In this work we particularly aim at the graphical representation of the periodic changes of the line of nodes.  相似文献   

17.
18.
19.
20.
We solve by an appropriate method the difficulty of near-commensurability, nn134, in the motion of Hyperion (Saturn VII) and give a first-order solution of its motion. Our result explains two interesting observed features, the regression of the apsidal line and the exclusive occurrence of apocentre C conjunction of SVII and SVI.  相似文献   

设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号