Method for determining roll rate gyro bias in an attitude heading reference system

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United States of America Patent

PATENT NO 7430460
APP PUB NO 20060217852A1
SERIAL NO

11088697

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Abstract

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A method and computer program product for determining the roll rate gyro bias of an attitude and heading reference system from true air speed, heading rate and body accelerations using centripetal force equations.

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Patent Owner(s)

Patent OwnerAddress
S-TEC CORPORATION DBA GENESYS AEROSYSTEMS1 S-TEC WAY MUNICIPAL AIRPORT MINERAL WELLS TX 76067

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Price, Ricardo A Boise, ID 3 140

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