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公开(公告)号:US09391366B2
公开(公告)日:2016-07-12
申请号:US13421678
申请日:2012-03-15
Applicant: Nicolas Martin , Jean-Michel Perre , Vincent Chopard
Inventor: Nicolas Martin , Jean-Michel Perre , Vincent Chopard
Abstract: The invention relates to a method for calibrating an antenna of a receiver of signals (s1, . . . , sN) originating from a plurality of sources, said receiver comprising a plurality of sensors (c1, . . . , cM), characterized in that it comprises the following steps: measurement of a phase shift (dm,n measure) for each of the sensors (c1, . . . , cM) on each of the signals (s1, . . . , sN), determination of at least one attitude value of the antenna, said attitude being defined by a set of coordinates, calculation, for each of the sensors on each of the signals, of a theoretical phase shift (dm,n theoretical) as a function of the attitude of the antenna, from the directions of arrival of the signals, calculation of a bias (β1 sensor m) for each of the sensors from the measured phase shifts (dm,n measure) and from the theoretical phase shifts (dm,n theoretical) of the sensor.
Abstract translation: 本发明涉及一种用于校准源自多个源的信号(s1,...,sN)的接收机的天线的方法,所述接收机包括多个传感器(c1,...,cM),其特征在于 它包括以下步骤:对每个信号(s1,...,sN)上的每个传感器(c1,...,cM)进行相移(dm,n测量)的测量, 至少一个天线的姿态值,所述姿态由一组坐标定义,对于每个信号中的每个传感器,计算理论相移(dm,n理论)的函数作为 天线,从信号的到达方向,从测量的相移(dm,n测量)和理论相移(dm,n理论)计算每个传感器的偏差(&bgr。1传感器m) 的传感器。
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公开(公告)号:US08378890B2
公开(公告)日:2013-02-19
申请号:US12969904
申请日:2010-12-16
Applicant: Vincent Chopard , Nicolas Martin
Inventor: Vincent Chopard , Nicolas Martin
Abstract: A satellite-based positioning receiver includes processing channels, each processing channel being associated with a respective satellite from among N satellites, and an extended Kalman filter for performing a vector tracking for the set of satellites using signals received from the satellites. The extended Kalman filter performs a resetting on the basis of the phase error and code error received directly from the phase and code discriminators, of each channel, and the receiver is configured for calculating the code-wise and carrier-wise control signals for the code phase and carrier phase numerically-controlled oscillators, on the basis of data provided by the extended Kalman filter, for each channel.
Abstract translation: 基于卫星的定位接收机包括处理信道,每个处理信道与N个卫星中的相应卫星相关联,以及扩展卡尔曼滤波器,用于使用从卫星接收的信号来执行卫星组的向量跟踪。 扩展卡尔曼滤波器基于每个信道的相位和码鉴别器直接接收到的相位误差和码错误执行复位,并且接收器被配置用于计算码的代码和载波控制信号 基于由扩展卡尔曼滤波器提供的数据,用于每个通道的相位和载波相位数字控制振荡器。
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公开(公告)号:US20130044027A1
公开(公告)日:2013-02-21
申请号:US13421678
申请日:2012-03-15
Applicant: Nicolas Martin , Jean-Michel Perre , Vincent Chopard
Inventor: Nicolas Martin , Jean-Michel Perre , Vincent Chopard
IPC: G01S19/23
Abstract: The invention relates to a method for calibrating an antenna of a receiver of signals (s1, . . . , sN) originating from a plurality of sources, said receiver comprising a plurality of sensors (c1, . . . , cM), characterized in that it comprises the following steps: measurement of a phase shift (dm,n measure) for each of the sensors (c1, . . . , cM) on each of the signals (s1, . . . , sN), determination of at least one attitude value of the antenna, said attitude being defined by a set of coordinates, calculation, for each of the sensors on each of the signals, of a theoretical phase shift (dm,n theoretical) as a function of the attitude of the antenna, from the directions of arrival of the signals, calculation of a bias (β1 sensor m) for each of the sensors from the measured phase shifts (dm,n measure) and from the theoretical phase shifts (dm,n theoretical) of the sensor.
Abstract translation: 本发明涉及一种用于校准源自多个源的信号(s1,...,sN)的接收机的天线的方法,所述接收机包括多个传感器(c1,...,cM),其特征在于 它包括以下步骤:对每个信号(s1,...,sN)上的每个传感器(c1,...,cM)进行相移(dm,n测量)的测量, 至少一个天线的姿态值,所述姿态由一组坐标定义,对于每个信号中的每个传感器,计算理论相移(dm,n理论)的函数作为 天线,从信号的到达方向,从测量的相移(dm,n测量)和理论相移(dm,n理论)计算每个传感器的偏差(&bgr。1传感器m) 的传感器。
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公开(公告)号:US20110181463A1
公开(公告)日:2011-07-28
申请号:US12969904
申请日:2010-12-16
Applicant: Vincent CHOPARD , Nicolas MARTIN
Inventor: Vincent CHOPARD , Nicolas MARTIN
Abstract: A satellite-based positioning receiver includes processing channels, each processing channel being associated with a respective satellite from among N satellites, and an extended Kalman filter for performing a vector tracking for the set of satellites using signals received from the satellites. The extended Kalman filter performs a resetting on the basis of the phase error and code error received directly from the phase and code discriminators, of each channel, and the receiver includes first means for calculating the code-wise and carrier-wise control signals for the said code phase and carrier phase numerically-controlled oscillators, on the basis of data provided by the said extended Kalman filter, for each channel.
Abstract translation: 基于卫星的定位接收机包括处理信道,每个处理信道与N个卫星中的相应卫星相关联,以及扩展卡尔曼滤波器,用于使用从卫星接收的信号来执行卫星组的向量跟踪。 扩展卡尔曼滤波器基于每个信道的相位和码鉴别器直接接收到的相位误差和码错误执行复位,并且接收机包括用于计算用于各个信道的代码和载波控制信号的第一装置 基于由所述扩展卡尔曼滤波器提供的数据,针对每个通道,所述码相位和载波相位数字控制振荡器。
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