Method and apparatus for improving the accuracy of position esti

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364459, 342357, 342358, 342457, G06F 1550

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active

053901240

ABSTRACT:
The accuracy of a vehicle position estimate generated using a satellite-based navigation system is improved by accounting for non-linear errors in the vehicle position computations. The standard navigation equation is modified to include the error coefficients .alpha., .beta., .gamma. and .delta.. .alpha. is used to model errors in the x dimension. .beta. is used to model errors in the y dimension. .gamma. is used to model errors in the z dimension. .delta. is used to model errors in the pseudoranges. The error coefficients may be computed using an open-ended GPS system or a differential GPS system. The error coefficients may be computed in real time or may be computed once and used for a period thereafter. Once computed, the error coefficients are factored into the computation of a vehicle position estimate for increased precision.

REFERENCES:
patent: 4667203 (1987-05-01), Counselman, III
patent: 4751512 (1988-06-01), Longaker
patent: 4870422 (1989-09-01), Counselman, III
patent: 4894662 (1990-01-01), Counselman
patent: 4912475 (1990-03-01), Counselman, III
patent: 5119102 (1992-06-01), Barnard
patent: 5148179 (1992-09-01), Allison
patent: 5155490 (1992-10-01), Spradley, Jr. et al.
"Compensating for GPS Ephemeris Error", NASA Tech Briefs, Nov. 1992, pp. 56 and 58.

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