Method and apparatus for detecting anomalies in landing...

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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07970503

ABSTRACT:
A method, apparatus, and computer program product for detecting anomalies in a landing system. In one embodiment, a magnitude difference between a blended inertial deviation magnitude and a raw deviation magnitude is identified to form a magnitude difference. The magnitude difference is compared to a magnitude threshold. If the magnitude difference exceeds the magnitude threshold, an anomaly in the data is detected.

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patent: 2005/0182530 (2005-08-01), Murphy
patent: 2006/0167619 (2006-07-01), Arethens
EP search report dated Apr. 4, 2010 for application EP08253010.

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