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Satellite search methods for improving time to first fix in a GPS receiver

  • US 5,402,347 A
  • Filed: 07/22/1993
  • Issued: 03/28/1995
  • Est. Priority Date: 07/22/1993
  • Status: Expired due to Term
First Claim
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1. A method for quickly obtaining a first positional fix after a short period of non-operation with a multiple channel GPS receiver having a local oscillator with a frequency uncertainty that exceeds an actual Doppler carrier frequency shift and adds to the total apparent Doppler frequency shift, the method comprising the steps of:

  • pre-computing a table of codes associated with a plurality of constellations of orbiting GPS satellites predicted to be visible at a plurality of times in the future based on a current time and a GPS satellite almanac and a predetermined geographic position of said GPS receiver with said table indexed according to said future times;

    fetching one part of said table of codes according to a time said GPS receiver is re-powered up after a period of power-off that followed the step of pre-computing said table;

    searching for a signal from a first GPS satellite associated with said fetched part of said table of codes in parallel using said multiple channels of said GPS receiver such that a first frequency search range is positioned with a nominal frequency estimated for said GPS satellite signal at its mid-point and a first GPS receiver channel is appointed to search said first frequency search range and a second GPS receiver channel is appointed to search in parallel a second frequency search range adjacent to said first frequency search range;

    splitting said multiple channels between searching for said first GPS satellite and a second GPS satellite if said first GPS satellite signal was not found; and

    using an offset frequency value for controlling said local oscillator obtained from locking onto a first-found GPS satellite signal in subsequent searches for other GPS satellite signals, wherein said local oscillator frequency uncertainty contribution to said total apparent Doppler frequency shift is substantially reduced in magnitude, and the time required to acquire a subsequent satellite signal is thus substantially reduced.

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