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FREQUENCY AIDING METHOD AND SYSTEM FOR NAVIGATION SATELLITE RECEIVER WITH CRYSTAL OSCILLATOR FREQUENCY HYSTERESIS

  • US 20090278735A1
  • Filed: 05/09/2008
  • Published: 11/12/2009
  • Est. Priority Date: 05/09/2008
  • Status: Active Grant
First Claim
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1. A navigation satellite receiver, comprising:

  • a crystal oscillator having an operable temperature range, the crystal oscillator adapted to generate an input clock signal having an actual frequency that drifts from a nominal frequency over the operable temperature range;

    a temperature sensor thermally coupled with the crystal oscillator for taking temperature measurements of the crystal oscillator;

    a navigation platform for receiving a plurality of signals having a known transmit frequency, the platform being capable of operating;

    in an acquisition mode in which the navigation platform attempts to receive, based on the input clock signal, at least one signal from at least one navigation satellite within a search window;

    in an operational mode, in which the navigation platform is adapted to receive, based on the input clock signal, a plurality of signals from different navigation satellites to obtain a current positional fix for the receiver; and

    a processor for producing first and second sets of frequency information, indicative of a discrepancy between the actual and the nominal frequency of the input clock signal, as a function of oscillator temperature measurements taken by the temperature sensor;

    whereby in acquisition mode, the navigation platform determines at least one parameter of the search window for a current oscillator temperature, based on the first and/or second sets of frequency information, to take into account any discrepancy between the actual frequency in relation to the nominal frequency of the input clock signal.

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