System and method for improving aircraft formation flying...

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

Reexamination Certificate

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Reexamination Certificate

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10891853

ABSTRACT:
An aircraft formation positioning system lead aircraft transmits a continuous RF signal and a periodic data burst with lead aircraft position. A follower aircraft receives the continuous RF signal and the periodic data burst. A follower aircraft resolver determines bearing, distance and elevation relative to the lead aircraft from the continuous RF signal. The follower aircraft transmits an intermittent RF signal and a periodic data burst with its relative position determined from the continuous RF signal. The lead aircraft receives the intermittent RF signal and the periodic data burst from the follower aircraft. A lead aircraft resolver performs an independent measurement of the lead aircraft position relative to the follower aircraft from the intermittent RF signal. A lead aircraft Kalman filter connected to the lead aircraft resolver and receiver correlates the independent measurement of the lead aircraft position relative to the follower aircraft with the received periodic data burst.

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patent: 6646588 (2003-11-01), Tran
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Patent Application for “Relative Navigation for Automated Aerial Refueling Using Datalink Signals” by Gary A. McGraw et al., filed May 19, 2004.
Patent Application for “Aircraft Formation/Refueling Guidance System” by Kenneth W. Mc Elreath, filed herewith.

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