US6011509A
Expired / Lapsed
US
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Apparatus and method for determination of a receiver position
Assignee: Raytheon Co
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Filing: 1999-05-25
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Granted: 2000-01-04
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Expires: 2019-05-25
Abstract
Abstract A method of accurate determination of a fixed position using global positioning system uses pseudo-range output over a predetermined measurement period from a stand-alone GPS receiver located at the fixed position, the pseudo-range output being measured from an ensemble of space vehicles at each time t over the measurement period, and historical ephemerides of the ensemble of space vehicles over the same measurement period to eliminate errors caused by selective availability. The historical ephemerides of the ensemble of space vehicles corresponding to each measurement time t are determined, and using the pseudo-range output and the historical ephemerides, a position solution at each time t is computed. The accurate position in earth-centered earth-fixed coordinates is then the average of all the position solutions at each time t over the measurement period.
Inventors
- 👤 Stephen C. Dutka
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 10:52
CPC Classifications
G; G01; G01S; G01S19/00; G01S19/38; G01S19/39; G01S19/42; G01S19/01; G01S19/13; G01S19/21; G01S19/215
Claims Analysis
Total Claims: 16
Claim 1
Independent Claim
102 words
A method of determination of a receiver fixed position using global positioning system (GPS), comprising: obtaining pseudo-range output over a predetermined measurement period from a GPS receiver, the pseudo-range output measured from an ensemble of space vehicles at each of a plurality of times t over the measurement period; determining the historical ephemerides of the ensemble of space vehicles corresponding to each of the plurality of times t; determining a position solution for each of the plurality of times t utilizing the pseudo-range output and the ephemerides; and averaging the position solution for each of the times t over the measurement period.
Claim 2
Independent Claim
102 words
A method of determination of a receiver fixed position using global positioning system (GPS), comprising: obtaining pseudo-range output over a predetermined measurement period from a GPS receiver, the pseudo-range output measured from an ensemble of space vehicles at each of a plurality of times t over the measurement period; determining the historical ephemerides of the ensemble of space vehicles corresponding to each of the plurality of times t; determining a position solution for each of the plurality of times t utilizing the pseudo-range output and the ephemerides; and averaging the position solution for each of the times t over the measurement period.
Claim 3
Dependent Claim
33 words
The method, as set forth in claim 1, wherein determining historical ephemerides comprises: determining an orbit defined by the historical ephemerides; and determining intermediate historical ephemerides between the historical ephemerides in the orbit.
Claim 4
Dependent Claim
20 words
The method, as set forth in claim 2, wherein determining the orbit comprises fitting an orbit to the historical ephemerides.
Claim 5
Dependent Claim
106 words
The method, as set forth in claim 1, wherein determining a position solution for each of the plurality of times t comprises; determining an initial receiver position; determining, in response to the historical ephemerides and the initial receiver position, a range from each space vehicle to the receiver; determining a difference between the range of each space vehicle and the receiver pseudo-range output; determining errors of the initial receiver position in response to the difference between the range of each space vehicle and the receiver pseudo-range output; correct the initial receiver position with the errors; and iteratively repeating the above steps until the errors approach zero.
Claim 6
Dependent Claim
39 words
The method, as set forth in claim 1, wherein averaging the position solutions comprises: summing all position solutions of each axis; and dividing the summed position solution for each axis by the number of position solutions in each axis.
Claim 7
Independent Claim
148 words
A method of determination of a receiver position using a stand-alone global positioning system (GPS) receiver, the receiver generating a plurality of pseudo-range data over a measurement period, comprising: receiving the plurality of pseudo-range data over the measurement period, the pseudo-range data measured for an ensemble of at least four space vehicles at each of a plurality of times t over the measurement period; receiving historical ephemerides of the same ensemble of space vehicles over the measurement period; determining from the received ephemerides an orbit for each space vehicle; determining intermediate historical ephemerides between the historical ephemerides in each orbit for each of the plurality of times t during the measurement period; determining a position solution for each of the plurality of times t utilizing the plurality of pseudo-range data and the ephemerides; and averaging the position solution for each of the times t over the measurement period.
Claim 8
Independent Claim
148 words
A method of determination of a receiver position using a stand-alone global positioning system (GPS) receiver, the receiver generating a plurality of pseudo-range data over a measurement period, comprising: receiving the plurality of pseudo-range data over the measurement period, the pseudo-range data measured for an ensemble of at least four space vehicles at each of a plurality of times t over the measurement period; receiving historical ephemerides of the same ensemble of space vehicles over the measurement period; determining from the received ephemerides an orbit for each space vehicle; determining intermediate historical ephemerides between the historical ephemerides in each orbit for each of the plurality of times t during the measurement period; determining a position solution for each of the plurality of times t utilizing the plurality of pseudo-range data and the ephemerides; and averaging the position solution for each of the times t over the measurement period.
Claim 9
Dependent Claim
20 words
The method, as set forth in claim 6, wherein determining the orbit comprises fitting an orbit to the historical ephemerides.
Claim 10
Dependent Claim
102 words
The method, as set forth in claim 6, wherein determining a position solution at each time t comprises: determining an initial receiver position; determining, in response to the historical ephemerides and the initial receiver position, a range from each space vehicle to the receiver; determining a difference between the range of each space vehicle and the receiver pseudo-range output; determining errors of the initial receiver position in response to the difference between the range of each space vehicle and the receiver pseudo-range output; correct the initial receiver position with the errors; and iteratively repeating the above steps until the errors approach zero.
Claim 11
Dependent Claim
39 words
The method, as set forth in claim 6, wherein averaging the position solutions comprises: summing all position solutions for each axis; and dividing the summed position solution for each axis by the number of position solutions in each axis.
Claim 12
Dependent Claim
129 words
A stand-alone global positioning system (GPS) receiver having a post-processor for accurate determination of a fixed position, the post-processor programmed to: receive a plurality of pseudo-range measurements over a predetermined measurement period, the pseudo-range measurements determined from an ensemble of space vehicles at each of a plurality of times t over the measurement period; obtain historical ephemerides of the ensemble of space vehicles over the measurement period, the historical ephemerides being free of the selective availability broadcast ephemeris error; determine the historical ephemerides of the ensemble of space vehicles corresponding to each time t in response to the obtained historical ephemerides; use the plurality of pseudo-range measurements and the historical ephemerides to determine a position solution at each time t; and average the position solutions over the measurement period.
Claim 13
Dependent Claim
129 words
A stand-alone global positioning system (GPS) receiver having a post-processor for accurate determination of a fixed position, the post-processor programmed to: receive a plurality of pseudo-range measurements over a predetermined measurement period, the pseudo-range measurements determined from an ensemble of space vehicles at each of a plurality of times t over the measurement period; obtain historical ephemerides of the ensemble of space vehicles over the measurement period, the historical ephemerides being free of the selective availability broadcast ephemeris error; determine the historical ephemerides of the ensemble of space vehicles corresponding to each time t in response to the obtained historical ephemerides; use the plurality of pseudo-range measurements and the historical ephemerides to determine a position solution at each time t; and average the position solutions over the measurement period.
Claim 14
Dependent Claim
36 words
The receiver, as set forth in claim 10, wherein the post-processor being further adapted to: determine an orbit defined by the obtained historical ephemerides; and determine intermediate historical ephemerides between the historical ephemerides in the orbit.
Claim 15
Dependent Claim
107 words
The receiver, as set forth in claim 10, wherein the post-processor is programmed to determine a position solution at each time t comprises: determining an initial receiver position; determining, in response to the historical ephemerides and the initial receiver position, a range from each space vehicle to the receiver; determining a difference between the range of each space vehicle and the receiver pseudo-range output; determining errors of the initial receiver position in response to the difference between the range of each space vehicle and the receiver pseudo-range output; correct the initial receiver position with the errors; and iteratively repeating the above steps until the errors approach zero.
Claim 16
Dependent Claim
45 words
The receiver, as set forth in claim 10, wherein the post-processor is further programmed to average the position solutions by: summing all position solutions in each axis; and dividing the summed position solution in each axis by the number of position solutions in each axis.
References Cited (Backward Citations)
US5523763A
Cited
US5451964A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 2003-01-03 | 2003-07-05 | 2004-01-04 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2007-01-03 | 2007-07-05 | 2008-01-04 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2011-01-03 | 2011-07-05 | 2012-01-04 | $7700.00 | Window Closed / Lapsed |