Method and apparatus for processing a satellite positioning system signal using a cellular acquisition signal

Abstract

Method and apparatus for processing satellite positioning system signals is described. In one example, assistance data is received at a mobile receiver from a first wireless network using a wireless transceiver. The first wireless network may be a non-synchronized cellular network. A time synchronization signal is obtained from a second wireless network at the mobile receiver using a wireless receiver. A time offset is then determined in response to the time synchronization signal. Satellite signals are processed at the mobile receiver using the assistance data and the time offset. The second wireless network may be a synchronized cellular network or may be a non-synchronized cellular network that is externally synchronized to GPS time.

Description

RELATED APPLICATIONS[0001]This application is a continuation of pending U.S. patent application Ser. No. 10 / 926,792, filed Aug. 26, 2004, which is a continuation-in-part of issued U.S. Pat. No. 7,053,824, issued May 30, 2006, which is incorporated by reference herein in its entirety.FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT[0002][Not Applicable][MICROFICHE / COPYRIGHT REFERENCE][0003][Not Applicable]BACKGROUND OF THE INVENTION[0004]Embodiments of the present invention generally relate to satellite position location systems and, more particularly, to a method and apparatus for receiving a global positioning system signal using a cellular acquisition signal.[0005]Global Positioning System (GPS) receivers use measurements from several satellites to compute position. GPS receivers normally determine their position by computing time delays between transmission and reception of signals transmitted from satellites and received by the receiver on or near the surface of the earth. The time d...

AI Technical Summary

Benefits of technology

[0014]Method and apparatus for processing satellite positioning system signals is described. In one embodiment, assistance data is received at a mobile receiver from a first wireless network using a wireless transceiver. The assistance data may comprise acquisition assistance data (e.g., expected pseudorange data), satellite trajectory data (e.g., satellite ephemeris), or both. The first wireless network may be a non-synchronized cellular network. A time synchronization signal is obtained from a second wireless network at the mobile receiver using a wireless receiver. A time offset is then determined in response to the time synchronization signal. Satellite signals are processed at the mobile receiver using the assistance data and the time offset. The second wireless network may be a synchronized cellular network (e.g., a CDMA network) or may be a non-synchronized cellular network that is externally synchronized to GPS time (e.g., a GSM network having location measurement units (LMUs)). The mobile receiver is thus configured to receive the time synchronization signal without a subscription to the second wireless network, which eliminates fees for such a subscription. In addition, the circuitry required for the receive-only front end is less complex and less costly than that required for a full transceiver.

Problems solved by technology

Absolute timing errors result in range errors of up to 0.8 m for each millisecond of timing error.

These range errors produce a similarly sized error in the GPS receiver position.

Hence, absolute time accuracy of 10 ms is sufficient for position accuracy of approximately 10 m. Absolute timing errors of much more than 10 ms will result in large position errors, and so typical GPS receivers have required absolute time to approximately 10 milliseconds accuracy or better.

As discussed above, an absolute time error of 1 millisecond leads to range errors of up to 0.8 meters while an absolute time error of 1 microsecond would cause an almost unobservable range error of less than 1 millimeter.

A common mode error of 1 microsecond, however, results in a pseudorange error of 1 microsecond multiplied by the speed of light (i.e., 300 meters).

Common mode errors have a large effect on pseudorange computations, and it is, in practice, very difficult to calibrate the common mode error.

In some GPS applications, the signal strengths of the satellite signals are so low that either the received signals cannot be processed, or the time required to process the signals is excessive.

In such systems, the GPS receiver cannot synchronize to GPS time without receiving and decoding TOW information from the satellites signals.

In low signal-to-noise ratio environments, TOW information is difficult, if not impossible, to decode.

Without accurate time-of-day information, the GPS receiver cannot provide an accurate time-tag for its measurements, thereby deleteriously affecting the accuracy of the position computed by the network.

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