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    • 2. 发明授权
    • Satellite navigation system using multiple antennas
    • 卫星导航系统采用多个天线
    • US07693659B2
    • 2010-04-06
    • US11190640
    • 2005-07-27
    • Kurt R. ZimmermanDave LawrenceMichael L. O'ConnorPaul Montgomery
    • Kurt R. ZimmermanDave LawrenceMichael L. O'ConnorPaul Montgomery
    • G01C21/00
    • G01S19/54G01C21/165G01S19/50
    • A satellite navigation system using multiple antennas for providing the position of multiple fiduciary points on an object even when fewer than four satellites are visible to some or all the antennas. Satellite signals from the multiple antennas are fed into at least one receiver. The receiver or receivers utilize constraint information, which is independent of the satellite signals. These external constraints are used to augment the signals received from the satellites, to obtain the position solution for each antenna. In a preferred embodiment, a common reference clock is used to provide an external constraint. Examples of other external constraints that can be used in the current invention are distance between the antennas, inertial measurement of attitude, rotational or linear position sensors, etc.
    • 一种使用多个天线的卫星导航系统,用于在物体上提供多个受信点的位置,即使对于一些或所有天线可见少于四颗卫星。 来自多个天线的卫星信号被馈送到至少一个接收机。 接收机或接收机利用独立于卫星信号的约束信息。 这些外部约束用于增加从卫星接收的信号,以获得每个天线的位置解。 在优选实施例中,使用公共参考时钟来提供外部约束。 可以在本发明中使用的其他外部约束的示例是天线之间的距离,姿态的惯性测量,旋转或线性位置传感器等。