Differential GPS landing system

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

701213, 701215, 34235706, 34235712, 342358, 455 121, G06F 1900

Patent

active

060674849

ABSTRACT:
A differential GPS landing system having at least three GPS receivers at known locations in spatial proximity to each other, wherein each GPS receiver independently receives GPS signals from the plurality of GPS satellites and at least three reference stations, wherein each reference station receives a signal from a different two of the at least three GPS receivers and calculates two separate differential corrections for each satellite, wherein each differential correction is independently calculated using the signals received from a different one of the two GPS receivers. The reference stations preferably average the two calculated differential corrections for each satellite to produce an averaged differential correction for each satellite. The system then validates the averaged differential correction for each satellite calculated by each reference station using two integrity monitors, wherein each integrity monitor receives the averaged differential corrections from a different two of the at least three reference stations, and each integrity monitor compares, with respect to each GPS satellite, the averaged differential corrections from the two of the at least three reference stations to produce a validated set of differential corrections, and broadcasts the averaged differential correction for each satellite calculated by one of the three reference stations. The preferred differential GPS landing system further includes a method that utilizes current differential correction error statistics, prior differential correction error statistics and a Bayesian interval estimation bounding process to provide an error bound on the broadcast differential corrections.

REFERENCES:
patent: 5361212 (1994-11-01), Class et al.
patent: 5436632 (1995-07-01), Sheynblat
patent: 5504492 (1996-04-01), Class et al.
patent: 5596328 (1997-01-01), Stangeland
patent: 5600329 (1997-02-01), Brenner
patent: 5608393 (1997-03-01), Hartman
patent: 5610616 (1997-03-01), Vallot et al.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Differential GPS landing system does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Differential GPS landing system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Differential GPS landing system will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1843485

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.