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SATELLITE NAVIGATION USING LONG-TERM NAVIGATION INFORMATION AND AUTONOMOUS ORBIT CONTROL

机译:利用长期导航信息和自主轨道控制进行卫星导航

摘要

An improved approach to satellite-based navigation (e.g., GPS) is provided. In one embodiment, a method includes determining a nominal orbital path of a navigation satellite. The method also includes transmitting ephemeris data corresponding to the nominal orbital path from the navigation satellite to a plurality of navigation devices. The method further includes determining an actual orbital path of the navigation satellite locally at the navigation satellite. In addition, the method includes determining a deviation between the actual orbital path and the nominal orbital path locally at the navigation satellite. The method also includes autonomously adjusting the actual orbital path locally at the navigation satellite to reduce the deviation between the actual orbital path and the nominal orbital path.
机译:提供了一种用于基于卫星的导航(例如,GPS)的改进方法。在一个实施例中,一种方法包括确定导航卫星的标称轨道路径。该方法还包括从导航卫星向多个导航设备发送与标称轨道路径相对应的星历数据。该方法还包括在导航卫星处本地确定导航卫星的实际轨道路径。另外,该方法包括在导航卫星处局部地确定实际轨道路径与名义轨道路径之间的偏差。该方法还包括在导航卫星处局部地自动调整实际轨道路径,以减小实际轨道路径与标称轨道路径之间的偏差。

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