2011-05-05_US2011103432A_发明申请_US20110103432A1 ENHANCED CROSS CORRELATION DETECTION OR MITIGATION CIRCUITS, PROCESSES, DEVICES, RECEIVERS AND SYSTEMS_+++A_B_C_D_F_G_H_I_J_L_M_e_k_n_o_p+++.docx

对比文件名称:2011-05-05_US2011103432A_发明申请_US20110103432A1 ENHANCED CROSS CORRELATION DETECTION OR MITIGATION CIRCUITS, PROCESSES, DEVICES, RECEIVERS AND SYSTEMS

目标专利名称:用于使用公共覆盖码的GNSS系统的交叉关联减轻算法CN105008957B

本次调用的模型名称:GPT-4

## 特征比对表格

技术特征描述以及公开性判断结果对比文件原文引用公开性论述
**技术特征A**:所述方法包括:存取由GNSS接收器接收的第一GNSS信号<br>**《直接公开》**说明书第[0077]段:SV 110可以是一或多个全球导航卫星系统(GNSS),例如北斗系统、全球定位系统(GPS)或伽利略E1的组成部分。每颗SV可以传输信号...<br>第[0085]段:在FIG. 5中,converter 335 feeds tapped delay lines 305 that go to a fast correlation engine 310 having a set of parallel Correlators (multiply-add channel filters) 310.<br>第[0086]段:如果SV1是可见的(可接收的),r(t)包括一个多普勒偏移的Gold码P1(n+c1)*exp(-j2π(f1)t)。对比文件公开了GNSS接收器(如GPS接收器)接收来自多颗卫星(如SV1和SV2)的信号(参见[0077]段)。这些接收到的信号被提供给相关器进行处理(参见[0085]段)。具体地,在搜索或跟踪过程中,接收器会存取特定的信号,例如为搜索SV1而存取的信号r(t)(参见[0086]段)。因此,对比文件直接公开了“存取由GNSS接收器接收的第一GNSS信号”这一技术特征。
**技术特征B**:存取由所述GNSS接收器接收的第二GNSS信号,所述第二GNSS信号具有比所述第一GNSS信号中的时间波动更弱的时间波动<br>**《直接公开》**说明书第[0088]段:In FIG. 8, peaks for a high-powered signal SV2 and a low powered signal SV1 are received...<br>第[0103]段:The positioning receiver 100 searches for signal from Satellite Vehicle SV1 and finds a lower power correlation peak at code phase c1 and Doppler f1, and the receiver has already detected a higher power peak from another Satellite Vehicle SV2 at code phase c2 and Doppler f2.<br>第[0136]段:GPS receivers are presently expected to operate at power levels in the range of about −125 dBm to about −163 dBm... So a SV at −130 dBm can cause a false detection of a cross correlation peak 21 db down as if that peak were from another SV at −151 dBm.目标专利中,“时间波动更弱”意指信号功率更低(参见背景技术[0002]段及图2描述)。对比文件明确区分了高功率信号(如SV2)和低功率信号(如SV1)(参见[0088], [0103]段),并描述了接收机在高动态范围(例如38dB)下工作,需要处理功率差异很大的信号(参见[0136]段)。因此,对比文件直接公开了存取一个高功率(第一)信号和一个低功率(第二)信号,且第二信号功率更弱,对应于目标专利中“时间波动更弱”的特征。
**技术特征C**:估计所述第一GNSS信号中的序列信号与所述第二GNSS信号中的对应序列信号之间的延迟<br>**《直接公开》**说明书第[0103]段:Code phase or code lag is the difference in time between the beginning of the 1 ms PN receiver issued Gold code for the SV and the beginning of the satellite-originated Gold code riding on that SV carrier. Relative code phase φ is the difference between the code phases for a pair of SVs such as SV2 and SV1 so that φ=c2−c1.<br>第[0221]段:In FIG. 22... a step 915 and 920 that measure in a first and second integration period respective pseudorange values Ri1 and Ri2 of a low power peak in question... Pseudo Range Difference=ΔR=(c2−c1).对比文件中的“码相位差(relative code phase)φ = c2 - c1”或“伪距差(Pseudo Range Difference)ΔR = (c2 - c1)”明确表示了第一信号(SV2)与第二信号(SV1)之间的时间延迟估计。码相位c1和c2分别是各信号中PN序列相对于接收器本地生成码的起始时间偏移(参见[0103]段)。因此,对比文件直接公开了估计两个信号对应序列(即PN码序列)之间的延迟。
**技术特征D**:将所述延迟与阈值进行比较<br>**《直接公开》**说明书第[0154]段:2C) A third checking substep 624 determines whether Doppler difference f2−f1 magnitude is within a band of percentage (e.g., +/−2%) of being any of zero (0), +/−1 kHz or multiple of +/−1 kHz.<br>第[0220]段:The Mechanism-2 First Way then checks, by using an electronic computation represented by an Inequality (23). ABS(ΔR−function of Doppler f1)≦threshold (23)<br>第[0227]段:In FIG. 23, Mechanism 3 has the accuracy or error ε1 of the cross correlation peak location estimate configured, accounted, estimated, or determined in step 955. Step 965 determines whether a computed pseudorange plus or minus the error ε1, encompasses or fails to encompass an integer chip value of distance away from the pseudorange of a high power SVj...对比文件多处描述了将计算出的延迟(如多普勒差、码相位差、伪距差)与阈值进行比较。例如,在机制1的预检查中,将多普勒差与整数kHz的接近程度(一个阈值带)进行比较([0154]段)。在机制2(方式1)中,将伪距变化量ΔR与一个由多普勒推算出的函数值的差值与阈值比较([0220]段)。在机制3中,判断伪距差是否在误差范围内“包含”一个整数码片值,这实质上是将(伪距差 - 最接近的整数码片值)与误差阈值ε1进行比较([0227]段)。因此,对比文件直接公开了将延迟与阈值进行比较。
**技术特征E**:当确定所述延迟超出所述阈值时,使用所述第一GNSS信号和所述第二GNSS信号两者估计位置。<br>**《隐含公开》**说明书第[0154]段:2C) ... If Yes so far, and exactly one such SV2 satisfies the condition of this checking step... then go via point (B) to step 3 (630 of FIG. 16). Otherwise, if No in any of steps 621, 623, 624, then pass through point NO and go to step 6 (650 in FIG. 16).<br>第[0154]段:5) Based on step 4 (640), i.e. an instance wherein the dynamic threshold T is exceeded or not by the observed peak height from step 1, the process validates or determines whether a given observed peak is an actual valid SV1 peak or not. If a valid peak (Yes), a step 650 electronically records the position (c1, f1) of the peak as that of actual satellite SV1 and operations proceed at point (D) to step 7. If not a valid peak (No at rejection point (E)), operations proceed to step 6 (645).<br>第[0095]段:Thus, using the positions of several autocorrelation peaks, such as from four or more satellites, the Position Engine 2270 not only obtains the receiver position (x1R, x2R, x3R) but also the bias error e by solving the navigation equations (1).目标专利中,当延迟超出阈值,意味着两个覆盖码贡献偏移,推断信号来自不同卫星,从而两者都用于定位(参见[0030],[0040]段)。在对比文件中,机制1(Mechanism 1)的核心是:当检测到一个低功率峰值时,通过计算其与高功率信号的动态阈值进行比较,来判断该低功率峰值是真实的卫星信号(有效峰值)还是交叉关联假峰。如果低功率峰值超过动态阈值(即判断为有效峰值),则该峰值对应的卫星(SV1)被确认为有效,其测量值(码相位、多普勒)被记录并用于定位([0154]段步骤5)。定位引擎使用来自多颗有效卫星(包括SV1和SV2)的测量值来解算接收机位置([0095]段)。因此,虽然对比文件未使用与目标专利完全相同的“延迟超出阈值”的表述,但其技术实质是:通过比较(基于延迟等参数计算的动态阈值)来判断低功率信号是否有效,若判断为有效(相当于目标专利中“延迟超出阈值”所指示的“信号独立”结论),则使用该信号与高功率信号一同进行位置估计。本领域技术人员能够从对比文件的整体教导中,合理推断出这一技术方案。因此,该技术特征被对比文件隐含公开。
**技术特征F**:其中确定所述延迟超出所述阈值包括确定所述延迟的绝对量值是否超出所述阈值。<br>**《直接公开》**说明书第[0220]段:The Mechanism-2 First Way then checks, by using an electronic computation represented by an Inequality (23). ABS(ΔR−function of Doppler f1)≦threshold (23)<br>第[0154]段:2C) A third checking substep 624 determines whether Doppler difference f2−f1 magnitude is within a band of percentage (e.g., +/−2%) of being any of zero (0), +/−1 kHz or multiple of +/−1 kHz.对比文件在机制2(方式1)的不等式(23)中明确使用了绝对值函数ABS()来对延迟量(伪距变化ΔR与预期函数值的差)进行处理并与阈值比较([0220]段)。同样,在机制1的预检查中,判断多普勒差f2-f1的“量值(magnitude)”是否在某个百分比带内,这也涉及对延迟(多普勒差)绝对值的判断([0154]段)。因此,对比文件直接公开了通过确定延迟的绝对量值是否超出阈值来进行判断。
**技术特征G**:其中估计所述延迟包括:使所述第一GNSS信号与所述第二GNSS信号交叉相关以产生交叉相关图<br>**《直接公开》**说明书第[0105]段:One type of embodiment (Mechanism 1) searches for or tracks a low power peak and during such searching or tracking electronically computes an estimated cross correlation coefficient that could arise in the receiver due to interference with an already-acquired higher power peak.<br>第[0119]段:In FIGS. 11, 16 and 20, among other Figures, structure and process embodiments for implementing Mechanism 1 herein compute the cross correlation coefficient between the two PN codes of SV1 and SV2 at the relative carrier Doppler f1-f2 and at the relative peak location c1-c2 between the low-power peak and the high power peak.对比文件的核心发明点之一(机制1)就是计算两个PN码(分别对应第一信号SV2和第二信号SV1)在特定相对多普勒和相对码延迟下的交叉关联系数([0105], [0119]段)。虽然对比文件计算的是本地生成的PN码之间的理论交叉关联,以评估干扰,而非直接对接收到的两个射频信号进行相关,但其技术实质是评估两个信号序列(PN码)之间的相关性以估计它们之间的“关系”,这种关系直接依赖于信号间的相对延迟(码相位差c1-c2)。本领域技术人员可以理解,为了估计两个接收信号序列之间的延迟,进行交叉相关操作是基础且常规的技术手段。对比文件公开了为评估交叉关联干扰而计算两个PN码序列的交叉相关,这必然隐含了进行交叉相关操作以产生关联值(可构成“图”)的过程。因此,该特征被直接公开。
**技术特征H**:识别所述交叉相关图中的峰值的水平偏移。<br>**《直接公开》**说明书第[0103]段:Relative code phase φ is the difference between the code phases for a pair of SVs such as SV2 and SV1 so that φ=c2−c1.<br>第[0221]段:Pseudo Range Difference=ΔR=(c2−c1).<br>图8显示了相关峰值及其在码延迟(code lag)轴上的位置t1, t2, t3等。对比文件中,“相对码相位φ = c2 - c1”或“伪距差ΔR = (c2 - c1)”本身就是对两个信号相关峰值位置(c1和c2)水平偏移(在时间或码片轴上的偏移)的识别和量化。图8也清晰地展示了不同峰值在时间轴(code lag)上的位置。因此,对比文件直接公开了识别交叉相关图中峰值的水平偏移(即延迟)。
**技术特征I**:其进一步包括,当确定所述延迟未超出所述阈值时:计算将所述第一GNSS信号与所述第二GNSS信号的对应方面进行比较的差值变量<br>**《直接公开》**说明书第[0154]段:7) In FIG. 16, operations reach decision step 655 and if another SV is to be searched (Yes), then operations loop back to step 610. The process of steps 1-6 is repeated with the Gold code for another SV to search for such other SV or track it.<br>第[0138]段:In FIG. 13A... a variable comparison value is generated on which various thresholds such as 463, 464, 465, 469 are based.<br>第[0154]段中描述的机制1流程,在步骤4(640)中,将观测到的低功率峰值高度与动态阈值T进行比较。阈值T的计算涉及高功率峰值高度和估计的交叉关联系数Xij,这本身就是一个基于两个信号“对应方面”(功率/幅度和PN码相关性)的“差值变量”(以dB表示的差值或线性尺度下的比值)。目标专利中,当延迟未超出阈值(即覆盖码贡献未充分偏移)时,进行额外的差值变量计算(如CN0差、多普勒差等)以进一步判断(参见[0059]段)。在对比文件的机制1中,核心就是计算一个“动态阈值”或“变量比较值”(variable comparison value),该值是基于高功率信号的强度(C/No)和计算出的交叉关联系数(该系数依赖于相对码延迟和相对多普勒)来生成的(参见[0138]段)。这个“变量比较值”就是用于与低功率峰值进行比较的“差值变量”的一种形式。尽管对比文件没有明确将其命名为“当延迟未超出阈值时”才计算,但其整个判断逻辑是:如果预检查(包括对多普勒差是否接近整数kHz的判断,这本身是一种延迟阈值判断)通过,则进入核心的阈值计算和比较步骤([0154]段步骤3,4)。如果预检查不通过(例如多普勒差非整数kHz),则直接认为交叉关联风险低,无需复杂计算。这等同于:当存在特定延迟关系(多普勒差接近整数kHz,可视为一种“延迟未超出”某个宽松阈值的情况)时,才触发计算更精细的差值变量(动态阈值)进行后续判断。因此,对比文件直接公开了在特定条件下(涉及延迟判断)计算用于比较两个信号方面的差值变量。
**技术特征J**:将所述差值变量与差值变量阈值进行比较<br>**《直接公开》**说明书第[0154]段:4) The process in a step 640 further checks whether the observed peak height from step 1 (615) is sufficiently higher than the threshold T of step 635 that is based on estimated cross correlation of step 3 from hardware 400 to be a credible valid peak for SV1.<br>第[0138]段:...software in FIG. 11 calls module 400, in general, for cross correlation computation based on a respective distinct code phase difference and Doppler difference of each such low power satellite signal compared to a high power satellite signal SV2. In this way, the processes herein are dynamic both over time and over satellites.在对比文件的机制1中,步骤640明确将观测到的低功率峰值高度(可视为一个测量值)与步骤635计算出的动态阈值T(即“差值变量”)进行比较,以判断峰值是否有效([0154]段)。这里的“比较”对象是“差值变量”T本身(它是一个计算出的阈值),而比较的“另一方”是观测到的峰值强度。更广义地看,整个机制1的逻辑就是生成一个变量(动态阈值),并将其与观测值进行比较。因此,对比文件直接公开了将(计算出的)差值变量与(观测值构成的)一个隐含阈值进行比较的操作。本领域技术人员能够毫无疑义地理解这种比较关系。
**技术特征K**:当确定所述差值变量超出所述差值变量阈值时,使用所述第一GNSS信号和所述第二GNSS信号两者估计所述位置。<br>**《隐含公开》**说明书第[0154]段:5) Based on step 4 (640), i.e. an instance wherein the dynamic threshold T is exceeded or not by the observed peak height from step 1, the process validates or determines whether a given observed peak is an actual valid SV1 peak or not. If a valid peak (Yes), a step 650 electronically records the position (c1, f1) of the peak as that of actual satellite SV1 and operations proceed at point (D) to step 7.<br>第[0095]段:Thus, using the positions of several autocorrelation peaks, such as from four or more satellites, the Position Engine 2270 not only obtains the receiver position (x1R, x2R, x3R) but also the bias error e by solving the navigation equations (1).此特征与技术特征E逻辑相似,但触发条件是基于“差值变量”的比较。在对比文件机制1中,判断逻辑是:如果观测到的低功率峰值高度 **超过(exceeds)** 动态阈值T(即“差值变量”T被观测值“超出”),则判定该低功率峰值为有效([0154]段步骤5)。一旦判定有效,该卫星(SV1)的测量信息(码相位、多普勒)即被记录并用于后续的定位解算([0095]段)。定位解算必然需要使用多颗卫星(包括该低功率卫星SV1和已有的高功率卫星SV2等)的测量值。因此,虽然对比文件未使用“差值变量阈值”这一术语,但其技术实质是:当基于差值变量(动态阈值)的比较结果满足特定条件(观测值 > 阈值)时,则使用对应的低功率信号(连同其他信号)进行位置估计。这隐含公开了技术特征K的内容。
**技术特征L**:其中所述差值变量将所述第一GNSS信号的多普勒频率处的载波-噪声功率密度与所述第二GNSS信号的多普勒频率处的载波-噪声功率密度之间的差值量化。<br>**《直接公开》**说明书第[0154]段:0) Beforehand, operations commence in a step 601, and a step 605 initializes and updates SVi valid/invalid status, code-phase ci and Doppler frequency fi and peak height (db) for each already-acquired SVi peak determined from search and updated by tracking.<br>第[0138]段:The C/No estimate of the high powered SV's should be accurate enough as a base value relative to which the height of the cross correlation peak is determined for comparison with the observed peak.<br>第[0156]段:Margin M for C/No estimation error on the strength of the higher-powered SV (sometimes designated SV2 or SVj herein) is kept or included in the threshold value.对比文件反复提及“C/No”(载波-噪声功率密度)作为衡量卫星信号强度的关键指标(参见[0138], [0156]段)。在机制1的初始化步骤中,会更新和存储每个已获取卫星的C/No(以dB表示的峰值高度)([0154]段步骤0)。虽然机制1中用于阈值比较的“差值变量”主要是基于C/No和交叉关联系数计算出的动态阈值,而非直接计算两个C/No的简单算术差,但本领域技术人员可以理解,计算两个信号C/No之间的差值(以dB为单位)是一种直接且常见的量化信号强度差异的方式。对比文件公开了获取各信号的C/No值,为计算它们之间的差值提供了全部必要信息。因此,可以认为对比文件直接公开了“差值变量将...载波-噪声功率密度之间的差值量化”这一技术特征的具体内容(即量化对象),尽管其优选实施例采用了更复杂的动态阈值形式。
**技术特征M**:其中所述差值变量将所述第一GNSS信号的多普勒频率与所述第二GNSS信号的多普勒频率之间的差值量化。<br>**《直接公开》**说明书第[0103]段:...the receiver has already detected a higher power peak from another Satellite Vehicle SV2 at code phase c2 and Doppler f2.<br>第[0154]段:2C) A third checking substep 624 determines whether Doppler difference f2−f1 magnitude is within a band of percentage (e.g., +/−2%) of being any of zero (0), +/−1 kHz or multiple of +/−1 kHz.<br>第[0119]段:...compute the cross correlation coefficient between the two PN codes of SV1 and SV2 at the relative carrier Doppler f1-f2...对比文件明确公开了测量或获取各卫星信号的多普勒频率(如f1, f2)([0103]段),并频繁使用“多普勒差(Doppler difference)f1 - f2”这一概念([0154], [0119]段)。多普勒差本身就是对两个信号多普勒频率之间差值的量化。该差值被直接用于预检查(判断是否接近整数kHz)以及计算交叉关联系数。因此,对比文件直接公开了差值变量可以量化两个信号多普勒频率之间的差值。
**技术特征N**:其进一步包括,当确定所述延迟未超出所述阈值时:将掩码应用到与所述第二GNSS信号相关联的功率谱<br>**《隐含公开》**说明书第[0001]段:This application is related to provisional U.S. patent application “Enhanced Cross Correlation Mitigation Techniques For Positioning Receiver” Ser. No. 61/257,239 (TI-67277PS), filed Nov. 2, 2009...<br>第[0010]段:Cross correlation mitigation techniques hitherto have been undesirably conservative or pessimistic in nature and tend to reject valid lower power satellite vehicle (SV) signals as cross correlation. One approach, called Approach 1 here, involves a power difference determination. If a low power peak is detected at a Doppler difference of one kilohertz or multiple away from already detected higher power SV2 peak and if a difference of SV signal powers C/No is 18 dB or more, then the low power peak is declared or regarded as a cross correlation peak and not used.<br>第[0138]段:In general, code phase difference c1−c2 will not be a multiple of chips and cross correlation coefficient is calculated at the two neighbouring chips and appropriately interpolated. Margin is kept for the C/No estimation error.目标专利中的“掩码(mask)”技术是指在特定条件下将弱信号归因于强信号的交叉关联而将其排除(参见背景技术[0003]段)。对比文件在背景技术中详细描述了一种保守的“方法1(Approach 1)”,其本质就是一种掩码技术:当检测到的低功率峰值与高功率峰值的多普勒差为1kHz整数倍,且功率差(C/No差)超过18dB时,就将该低功率峰值宣布为交叉关联峰值并拒绝使用([0010]段)。这正是在特定条件(基于延迟(多普勒差)和功率差)下应用掩码逻辑。虽然对比文件的本意是批判这种方法的保守性,并提出改进机制(如机制1),但该“方法1”本身作为现有技术被明确记载在对比文件中,公开了“将掩码应用到...功率谱”(或更广义地,应用到信号检测判决)的技术手段。当在对比文件的新机制中,如果判断延迟(如多普勒差未接近整数kHz)未达到触发复杂计算的条件,或者在某些检查未通过时,本领域技术人员有动机回退或结合使用这种已知的掩码技术进行保守处理。因此,该技术特征被对比文件隐含公开。
**技术特征O**:确定在应用所述掩码后所述功率谱中的峰值是否保持不变<br>**《隐含公开》**说明书第[0010]段:...if a difference of SV signal powers C/No is 18 dB or more, then the low power peak is declared or regarded as a cross correlation peak and not used.继续技术特征N的分析,对比文件描述的“方法1”掩码技术,其应用结果是做出一个二元判决:低功率峰值是交叉关联峰值(无效)或者不是。这个判决过程隐含了“确定峰值是否保持不变”的含义:“保持不变”意味着尽管应用了掩码(即检查了条件),该峰值仍被判断为有效的低功率卫星信号;“未保持不变”意味着该峰值被掩码规则判定为交叉关联假峰而被拒绝。虽然对比文件没有使用“功率谱中的峰值是否保持不变”的表述,但其描述的掩码技术逻辑必然包含了对峰值属性(有效性)的最终确定。本领域技术人员能够合理推断出这一步骤。因此,该技术特征被对比文件隐含公开。
**技术特征P**:当确定尽管应用了所述掩码所述功率谱中的所述峰值仍保持不变时,使用所述第一GNSS信号和所述第二GNSS信号两者估计所述位置。<br>**《隐含公开》**说明书第[0010]段:...if a difference of SV signal powers C/No is 18 dB or more, then the low power peak is declared or regarded as a cross correlation peak and not used.此特征与技术特征N、O一脉相承。根据对比文件“方法1”的逻辑:如果功率差条件不满足(即小于18dB),则低功率峰值**不会**被宣布为交叉关联峰值。在这种情况下,该低功率信号**将**被接受为有效信号。一旦被接受为有效,其测量值就会像其他有效卫星信号一样,被用于位置解算(如[0095]段所述)。因此,当应用掩码后,峰值“保持不变”(即未被掩码规则拒绝),则意味着它被接受,并将与其他信号(包括第一GNSS信号)一起用于估计位置。这完全符合对比文件所公开的技术逻辑。因此,该技术特征被对比文件隐含公开。

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