(USPTO)The Patent Description & Claims data below is from USPTO Patent Application 20070247354. Brief Patent Description - - CROSS-REFERENCE TO RELATED PATENT APPLICATIONS[0001] This specification is related to and claims the benefit of U. S. Provisional Application No. 60/794,102 filed Apr. 24. 2006 which is hereby incorporated by reference. This specification is further related to U. S. Provisional Applications No. 60/815,838 filed Jun. 23. 2006 and 60/888,232 filed Feb. 5. 2007 both of which are also hereby incorporated by reference. BACKGROUND OF THE INVENTION[0002] The present invention relates generally to the field of Global Navigation Satellite Systems (GNSS) for navigation such as the Global Positioning System (GPS) or Galileo.[0003] In a GNSS system satellites in orbit around the Earth broadcast signals that can be received by a receiver equipped to detect them. The signals are transmitted such that a receiver can determine under adequate signal conditions the time of transmission of the signal. By receiving four such signals the receiver can determine the local time and its own position in a three-dimensional coordinate system.[0004] Such systems often rely on the ability to determine the distance between a satellite and a receiver. By knowing three such distances an accurate estimate of position can be made by determining the most likely intersection point of three spheres each centered on a particular satellite and having a radius equal to the measured distance from the satellite to the receiver.[0005] In order to make such a position determination it is of course necessary for the receiver to have an estimate of each satellite's location. Such location estimates are generated with the help of satellite ephemeris data which is data that is usable to estimate a satellite's position.[0006] Such satellite ephemeris data is generally stored in the form of parameters which can be used in a known model of the satellite's orbit to generate a position estimate as a function of time. For example the ephemeris calculations for GPS are described in the document GPS-ICD-200C which is hereby incorporated by reference.[0007] Ephemeris data in the GPS system for example are broadcast by each satellite and come in two forms. First. GPS satellites broadcast "almanac data" which are a form of ephemeris data although they are not generally referred to as such in the art. Almanac data are intended to be used to determine a rough estimate for a satellite's position for a period of more than a few hours after downloading. This can be useful for the receiver for example to determine which satellites are in the receiver's field of view if the receiver also has a rough estimate of its own position. Almanac data are typically accurate for a few months to within a few kilometers.[0008] GPS satellites also broadcast a more precise set of data referred to as "ephemeris data". GPS ephemeris data are typically accurate for a few hours to within a few meters. After a few hours the accuracy of this data degrades rapidly however.[0009] Both GPS almanac and GPS ephemeris data are broadcast by each satellite as part of a navigation data message that is superimposed upon a CDMA pseudorandom noise code. The ephemeris data for a particular satellite take typically (open sky--no visibility interruption) 30seconds to download. They cannot be downloaded if the signal is weak (less than -145 dBm). In weak signal conditions ephemeris data are typically transmitted to the (A)-GPS receiver from an assistance network. Under low signal power conditions such as those experienced indoors it is often very difficult to recover the GPS navigation message and thus to recover GPS ephemeris data. This means that GPS receivers which have not been allowed a clear view of the sky for several hours will experience a degradation in their position solution accuracy based on inaccurate estimates of each satellite's current position.[0010] Thus when a vehicle with a PND (Portable Navigation Device) or GPS receiver mounted on the dashboard or the windshield is parked overnight in an indoor garage the GPS functions usually cannot deliver a position until quite a long time after the vehicle leaves the garage the next day. The ephemeris data are outdated because of the GPS OFF duration of more than 4 hours (the usual maximum validity period for broadcast ephemerides). Here the term "valid" means producing an error within a preset tolerance. The GPS section takes a long time (up to 10 minutes) in urban canyon environments to recover the broadcast ephemerides from the satellites due to the low signal level conditions and the often highly interrupted nature of the received signals. No fix is possible until the broadcast ephemerides are recovered even if the satellites are tracked.[0011] Thus there is currently a need to extend and improve the accuracy of ephemeris data and the length of time during which ephemeris data can provide an accurate solution. SUMMARY OF THE INVENTION[0012] One embodiment of the invention relates to a method for improving the accuracy of a receiver position comprising applying a correction to almanac data. Optionally the method may be so performed that the step of applying a correction to almanac data comprises obtaining a correction term from a prediction file and applying the term to an estimated satellite position. The method may also be performed such that a corrected estimated satellite position with an accuracy of few meters results less than 30 meters but preferably less than 5 meters from the step of applying a correction to almanac data accurate to within about two kilometers. Preferably the correction is based on data which is received from a network; and the data allows the corrected estimated satellite position to be made accurate to within few meters within seven days after a reception time of the data from the network.[0013] Certain embodiments of the invention relate to a method for generating an extended ephemeris prediction file comprising: obtaining data comprising a prediction of a satellite orbit; computing correction terms related to a difference between the prediction of a satellite orbit and a second prediction resulting from almanac data; and wherein the prediction file is valid for at least seven days and comprises less than 60480 Bytes. The method can optionally be carried out such that the step of computing correction terms related to a difference between the prediction of a satellite orbit and a second prediction resulting from almanac data further comprises using both a harmonic model and a polynomial model. The method can further comprise the step of computing correction terms for satellite clock data and the step of transmitting the prediction file over a SUPL network. Preferably the prediction file comprises less than one kilobyte per day of validity. In a preferred embodiment the step of computing correction terms related to a difference between the prediction of a satellite orbit and a second prediction resulting from almanac data further comprises applying a least squares methodology to minimize the difference between the prediction of satellite orbit and the second prediction and further comprises weighting data from the prediction of satellite orbit that is further in the future less than data from the prediction of satellite orbit that is nearer in the future.[0014] Still further embodiments of the invention relate to a computer readable medium having computer code embedded therein that when executed would carry out a method for generating an extended ephemeris prediction file comprising: obtaining data comprising a prediction of a satellite orbit; computing correction terms related to a difference between the prediction of a satellite orbit and a second prediction resulting from almanac data; wherein the prediction file is valid for at least seven days and comprises less than 60480 Bytes. The method carried out by the instructions can be such that the step of computing correction terms related to a difference between the prediction of a satellite orbit and a second prediction resulting from almanac data further comprises using both a harmonic model and a polynomial model. Optionally the method carried out by the instructions further comprises the step of computing correction terms for satellite clock data and transmitting the prediction file over a SUPL network. In a preferred embodiment the prediction file comprises less than one kilobyte per day of validity. Preferably the step of computing correction terms related to a difference between the prediction of a satellite orbit and a second prediction resulting from almanac data further comprises applying a least squares methodology to minimize the difference between the prediction of satellite orbit and the second prediction and weighting data from the prediction of satellite orbit that is further in the future less than data from the prediction of satellite orbit that is nearer in the future.[0015] Still other embodiments of the invention relate to a GNSS receiver comprising: a communications port for receiving an almanac correction model; a memory for storing almanac data; circuitry for receiving GNSS signals; and a processor for calculating the position of the receiver based on the received GNSS signals and the position of a GNSS transmitter as calculated from almanac data and the almanac correction model. Optionally the processor for calculating the position of the receiver based on the received GNSS signals and the position of the GNSS transmitters as calculated from almanac data and the almanac correction model is configured to calculate a corrected estimated GNSS transmitter position based on a harmonic correction model and a polynomial correction model. BRIEF DESCRIPTION OF THE DRAWINGS[0016] FIG. 1 shows a first extended ephemeris prediction file system flow.[0017] FIG. 2 shows a second extended ephemeris prediction file system flow[0018] FIG. 3 shows a third extended ephemeris prediction file system flow[0019] FIG. 4 shows a system useful for extended ephemeris use. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTSContinue reading... Brief Patent Description - - Click on the above for other options relating to this Ephemeris extension method for gnss applications patent application.###
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