首页> 外国专利> DEVICE MODULE FOR THE DETECTION OF TEMPERATURE COMPENSATED CRYSTAL OSCILLATOR ORIGINATED MICRO-JUMPS IN A GLOBAL NAVIGATION SATELLITE SYSTEM AND RELATED DETECTION METHOD

DEVICE MODULE FOR THE DETECTION OF TEMPERATURE COMPENSATED CRYSTAL OSCILLATOR ORIGINATED MICRO-JUMPS IN A GLOBAL NAVIGATION SATELLITE SYSTEM AND RELATED DETECTION METHOD

机译:全球导航卫星系统中温度补偿晶体振荡器起源的微跳的检测模块及检测方法

摘要

A device for the detection of Temperature Compensated Crystal Oscillator originated micro-jumps in a GNSS (Global Navigation Satellite System) receiver (100), said receiver (100) comprisinga radio frequency stage (2) associated to a Temperature Compensated Crystal Oscillator (2a) to down convert received satellite signals (S1, ...SNS) as a function of the frequency of Temperature Compensated Crystal Oscillator (2a),an analog digital conversion module (3) to obtain digital signals from the down converted satellite signals,an acquisition module (4) including correlators (41) to identify in the digital signals satellites in visibility and provide corresponding GNSS information, in particular code and frequency information, supplying samples of in phase and quadrature components (I,Q) of said GNSS information to atracking module (5), comprising a plurality of tracking channels (TRK0...TRKNS-1) comprising a frequency or phase locked loop (513, 514) adjusting a tracking numerical controlled oscillator (54) which frequency is used to demodulate said GNSS information, said tracking module (5) including accumulating (511) over an accumulation period (k) having the bit length of the GNSS information and mixing (512) between consecutive bits to produce mixed quantities (IMIX, QMIX) which are used to compute an averaged phase rate (Δφ) used as set point of said frequency or phase loop (513, 514).;The device module comprisesa feeder module (210) configured to mix the information in the in phase and quadrature components (I,Q) inside the bit time frame of the GNSS information, to obtain a wide band phase (Δφ10) and configured to obtain a previous carrier to noise ratio estimate (Cn0*k-1) value, available on the channel from accumulation over the previous accumulation period (k-1),a vector table module (220), configured to store the wide band phase (Δφ10) and the previous carrier to noise ratio estimate (Cn0*k-1) value for each tracking channel (TRKi) of the tracking module (5), the feeder module (210) being configured to populate said vector table module (220) with said wide band phase (Δφ10) and previous carrier to noise ratio estimate (Cn0*k-1) value,a global monitor module (230) configured to scan (300) the vector table module (220) and to detect the occurrence of a micro-jump on the basis of the values of the wide band phase (Δφ10) and previous carrier to noise ratio estimate (Cn0*k-1) present for each tracking channel (TRKi) in said vector table module (220), said global monitor module (230) being further configured to compute (350) an amount (Δf) of said detected micro-jump and use said amount to update said tracking numerical controlled oscillator (54).
机译:一种用于检测GNSS(全球导航卫星系统)接收机(100)中的温度补偿晶体振荡器引起的微跳的设备,所述接收机(100)包括与温度补偿晶体振荡器(2a)相关联的射频级(2),以将接收到的卫星信号(S 1 ,... S NS )下转换为一个函数温度补偿晶体振荡器(2a)的频率,模拟数字转换模块(3),用于从降频后的卫星信号中获取数字信号,包括相关器(41)的获取模块(4),以在可见性中识别数字信号卫星并提供相应的GNSS信息,特别是代码和频率信息,提供所述GNSS信息的同相和正交分量(I,Q)的样本到跟踪模块(5),包括多个跟踪通道(TRK 0 ... TRK NS-1 ),包括频率或锁相环(513、514)进行调整跟踪数控振荡器(54),其频率用于解调所述GNSS信息,所述跟踪模块(5)包括在具有GNSS信息的比特长度的累加周期(k)上累加(511),并在之间进行混合(512)连续位以产生混合量(I MIX ,Q MIX ),这些混合量用于计算平均相位速率(Δφ )用作所述频率或相位环路(513、514)的设定点。馈线模块(210),被配置为将信息混合在GNSS信息的比特时间帧内的同相和正交分量(I,Q)中,以获得宽带相位(Δφ 10 )并配置为获得先前的载波噪声比估计值(Cn0 * k-1 )值,该值可从通道上的先前累积周期(k-1)的累积中获得,向量表模块(220),被配置为存储宽带相位(Δφ 10 )和先前的载波噪声比估计值(Cn0 * k-1跟踪模块(5)的每个跟踪通道(TRK i )的)值,馈送模块(210)配置为用所述宽带填充所述矢量表模块(220)相位(Δφ 10 )和先前的载波噪声比估计(Cn0 * k-1 )值,全局监控器模块(230),其配置为扫描(300)向量表模块(220),并根据宽带相位(Δφ所述向量表中每个跟踪通道(TRK i )的 10 )和先前的载波噪声比估计值(Cn0 * k-1 )模块(220),所述全局监控器模块(230)还被配置为计算(350)所述检测到的微跳的量(Δf),并使用所述量来更新所述跟踪数控振荡器(54)。

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