SATELLITE-BASED POSITIONING SYSTEM IMPROVEMENT

• US 20090102709A1
• Filed: 03/08/2008
• Published: 04/23/2009
• Est. Priority Date: 10/04/2002
• Status: Abandoned Application

• Current Assignee: U-Blox AG (u-blox Holding AG)
• Original Assignee: U-Blox AG (u-blox Holding AG)
• Inventors: Glennon, Eamonn P., BRYANT, Roderick C., Dougan, Stanley L., Dempster, Andrew G., Hobbs, Trevor
• Application Number:
  US12/044,969
• Publication Number:
  US 20090102709A1
• Time in Patent Office: Days
• US Class Current: 342/357.250
• CPC Class Codes: G01S 19/05 providing aiding data
• CPC Class Codes: G01S 19/06 employing an initial estimate of the location of the receiver as aiding data or in generating aiding data
• CPC Class Codes: G01S 19/23 Testing, monitoring, correcting or calibrating of receiver elements
• CPC Class Codes: G01S 19/24 Acquisition or tracking or demodulation of signals transmitted by the system synchronisation aspects of direct sequence spread spectrum modulation H04B1/7073
• CPC Class Codes: G01S 19/25 involving aiding data received from a cooperating element, e.g. assisted GPS
• CPC Class Codes: G01S 19/27 creating, predicting or correcting ephemeris or almanac data within the receiver
• CPC Class Codes: G01S 19/42 Determining position
• CPC Class Codes: G01S 5/10 Position of receiver fixed by co-ordinating a plurality of position lines defined by path-difference measurements , e.g. omega or decca systemsG01S5/12 takes precedence ; beacons and receivers cooperating therewith G01S1/306, G01S1/308
• CPC Class Codes: H04B 2201/70715 with application-specific features

Abstract

A method, device and system for determining a receiver location using weak signal satellite transmissions. The invention involves a sequence of exchanges between an aiding source and a receiver that serve to provide aiding information to the receiver so that the receiver'"'"'s location may be determined in the presence of weak satellite transmissions. With the aiding information, the novel receiver detects, acquires and tracks weak satellite signals and computes position solutions from calculated pseudo ranges despite the inability to extract time synchronization date f, '"'"'n the weak satellite signals. The invention includes as features, methods and apparatus for the calibration of a local oscillator, the cancellation of cross correlations, a Doppler location scheme, an ensemble averaging scheme, the calculation of almanac aiding from a table of orbit coefficients, absolute time determination, and a modified search engine.

Claims

1. In an SPS system for identifying the location of a receiver in the presence of satellite signal attenuation having a plurality of orbital satellites sending synchronized encoded signals on a carrier frequency wherein said encoded signals have repeated epochs containing synchronization data:

a receiver for detecting, acquiring, and tracking a set of the encoded signals and simultaneously determining the code phases of said set with respect to said epochs;

an aiding source to transmit information to the SPS system, and

wherein said receiver is comprised of a processor executing an algorithm for computing an initial approximate location from measured satellite Doppler differences.

2. The SPS system for identifying the location of a receiver in the presence of satellite signal attenuation of claim 1 wherein the receiver is comprised of a local oscillator and the algorithm executed by the processor has no dependence on a current local oscillator offset.

3. A method for identifying the location of a receiver in the presence of satellite signal attenuation of claim 1 wherein an SPS system executes a Doppler positioning algorithm comprising the steps of

applying space vehicle (SV) clock corrections to both the satellite time of transmit and the satellite Doppler frequency for each input observation made by the GPS receiver.

calculating satellite positions at the corrected satellite time of transmit estimating the receiver location,

establishing a threshold level for residual error;

and

iterating between the satellite range-rate and correcting the current estimate of the user position until a residual error in receiver location is below said threshold level.

4-5. -5. (canceled)

6. A method of calibrating a local oscillator of an SPS receiver comprising the steps of counting local oscillator cycles and fractions thereof over a period precisely determined by a number of signal framing intervals, calculating a calibration offset and using the calibration offset to correct the oscillator frequency

7. The method of calibrating a local oscillator of an SPS receiver of claim 6, wherein the calibration offset is used to correct the oscillator frequency so as to minimize the offset.

8. An SPS system for identifying the location of a receiver in the presence of satellite signal attenuation comprising:

a plurality of orbital satellites sending synchronized encoded signals on a carrier frequency wherein said encoded signals have repeated epochs containing synchronization data;

a receiver for detecting, acquiring, tracking a set of the encoded signals and simultaneously determining the code phases of said set with respect to said epochs;

an aiding source to transmit information to the SPS system, a canceler for reducing the amplitude of strong signals wherein the canceler is integrated into a correlator.

9. The SPS system for identifying the location of a receiver of claim 8, wherein a canceling finger is provided for each channel for which canceling is to be performed and said canceling finger takes one input from the code generator input to a prompt finger of a channel tracking a jamming signal and a second input from a code generator input of the finger for which cancellation is to be performed.

10. The SPS system for identifying the location of a receiver of claim 8 wherein the cancellation is performed at a point where the signal is represented by approximately 10 bits.

11-18. -18. (canceled)

19. An SPS system for identifying the location of a receiver in the presence of satellite signal attenuation comprising:

a plurality of orbital satellites sending synchronized encoded signals on a carrier frequency wherein said encoded signals have repeated epochs containing synchronization data;

a receiver for detecting, acquiring, tracking a set of the encoded signals and simultaneously determining the code phases of said set with respect to said epochs; and

a search engine having a search range of at least 60 chips after acquisition of the first satellite.