NAVIGATION SATELLITE ORBIT AND CLOCK DETERMINATION WITH LOW LATENCY CLOCK CORRECTIONS

In accordance with the received reference receiver measurement information, the system determines narrow-lane navigation solutions for the plurality of reference receivers (604). The system also determines, in accordance with the narrow-lane navigation solutions, at a first update rate, an orbit correction for each satellite (608); at a second update rate, a clock correction for each such satellite (610); and at a third update rate that is faster than the second update rate, an update to the clock correction for each such satellite (612). Further, the system generates navigation satellite corrections for each such satellite (614), including the orbit correction updated at the first update rate, and the clock correction that is updated at the third update rate. 根据所接收的参考接收器测量值信息，系统确定(604)用于多个参考接收器的窄巷导航解析值。该系统还根据窄巷导航解析值以第更新速率确定用于每个卫星(608)的轨道校正值；以第二更新速率确定用于每个此种卫星的时钟校正值(610)；以比第二更新速率快的第三更新速率确定用于每个此种卫星的对时钟校正值做出的更新(612)。此外，系统生成(614)用于每个此种卫星的导航卫星校正值，其包括以第更新速率被更新的轨道校正值和以第三更新速率被更新的时钟校正值。