Navigation system

Communications: directive radio wave systems and devices (e.g. – Determining distance – Altimeter

Reexamination Certificate

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Details

C342S122000

Reexamination Certificate

active

11018886

ABSTRACT:
A radar altimeter system with a closed-loop modulation for generating more accurate radar altimeter values. The present invention combines flight safety critical sensors into a common platform to permit autonomous or semi-autonomous landing, enroute navigation and complex precision approaches in all weather conditions. An Inertial Navigation System (INS) circuit board, a radar altimeter circuit board and a Global Navigation Satellite System (GNSS) circuit board are housed in a single chassis. VHF (Very High Frequency) Omni-directional Radio (VOR), Marker Beacon (MB), and VDB (VHF Data Broadcast) receiver circuit boards may also be implemented on circuit boards in the chassis.

REFERENCES:
patent: 5714948 (1998-02-01), Farmakis et al.
patent: 6426717 (2002-07-01), Maloratsky
patent: 2003/0093187 (2003-05-01), Walker
patent: 2006/0049977 (2006-03-01), Vacanti

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