Integration of aime augmentation into GNSS products

Details Integration of aime augmentation into GNSS products Integration of aime augmentation into GNSS products

1997-07-29

1999-10-19

Tarcza, Thomas

Communications: directive radio wave systems and devices (e.g.,

Directive

Including a satellite

701200, H04B 7185

Patent

active

059696680

ABSTRACT:
A global navigation satellite system (GNSS) receiver for use in an aircraft is disclosed. The GNSS receiver includes receiver circuitry for receiving satellite signals containing satellite data from a multiple GNSS satellites. The receiver circuitry generates a first navigation solution for the aircraft as function of the satellite data. A first GNSS receiver output couples to an inertial reference system (IRS) and provides the satellite data to the IRS. The IRS generates a second navigation solution for the aircraft as a function of the satellite data and as a function of IRS position data. A first GNSS receiver input couples to the IRS and receives the second navigation solution from the IRS. The GNSS receiver provides at a second output aircraft position information as a function of the second navigation solution.

REFERENCES:
patent: 5512903 (1996-04-01), Schmitke
patent: 5543804 (1996-08-01), Buchler et al.
patent: 5583774 (1996-12-01), Diesel
patent: 5714948 (1998-02-01), Farmakis
AIME, Your Path to GPS Sole Means, Litton Aero Products.
John Diesel and Gregory Dunn, GPS/IRS AIME: "Certification for Sole Means and Solution to RF Interference", Litton Aero Products.

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