U.S. patents available from 1976 to present.
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Centimeter accurate global positioning system receiver for on-the-fly real-time kinematic measurement and control

Patent 5890091 Issued on March 30, 1999. Estimated Expiration Date: Icon_subject February 19, 2018. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

Grading system
Patent #: 4807131
Issued on: 02/21/1989
Inventor: Clegg

Method of determining mining progress in open cast mining by means of satellite geodesy
Patent #: 5144317
Issued on: 09/01/1992
Inventor: Duddek, et al.

Agricultural aircraft control system using the global positioning system
Patent #: 5334987
Issued on: 08/02/1994
Inventor: Teach

Method and apparatus for operating compacting machinery relative to a work site Patent #: 5471391
Issued on: 11/28/1995
Inventor: Gudat, et al.

Inventors

Assignee

Application

No. 027827 filed on 02/19/1998

US Classes:

701/215, Having multiple GPS antennas or receivers (e.g., differential GPS)342/357.12, GPS receiver signal processing342/457Land vehicle location (e.g., bus, police car

Examiners

Primary: Zanelli, Michael J.

Attorney, Agent or Firm

International Classes

G01S 003/02
G01S 005/02
G06F 165/00

Abstract

A system embodiment of the present invention comprises a fixed and a roving pair of four-observable GPS receivers and a communication link between them for double differencing code and carrier measurements. Carrier phase integer ambiguities are resolved efficiently by searching the simultaneous narrow-lane intersections of both the L1 and L2 wave fronts propagated by the GPS satellites being tracked. External constraint information, such as elevation, is additionally used to speed up integer ambiguity resolution. Data between the reference station and the rover is communicated in compressed form at a regular interval, e.g., once a second at each epoch, and demi-measurements of carrier phase are obtained more frequently, e.g., ten times a second, and used to propagate solutions between epochs.

Other References

  • Remondi; "On-the-Fly" GPS Results Using Full-Wavelength Dual-Frequency Carrier Ranges; No Dat
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