Redundant system for the indication of heading and attitude...

Measuring and testing – Navigation – Ship's log

Reexamination Certificate

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C073S179000, C073S170020

Reexamination Certificate

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06955082

ABSTRACT:
A method for synthetically calculating redundant attitude and redundant heading for an aircraft using data existing in the aircraft, including angular rates p, q, r around x-, y- and z-coordinates of an aircraft-fixed (body frame) coordinate system, air data information including speed, altitude and angle of attack, includes the steps of calculating attitude and heading based on the body-frame angular rates p, q, r, estimating errors in measured body-frame magnetic field vector components, deriving a measured body-frame field magnetic field vector, estimating errors in calculated attitude and heading using the air data and the derived measured body-frame magnetic field vector components, and correcting the calculated attitude and heading using the estimated errors in attitude and heading.

REFERENCES:
patent: 4106094 (1978-08-01), Land
patent: 4254465 (1981-03-01), Land
patent: 4914598 (1990-04-01), Krogmann et al.
patent: 5841537 (1998-11-01), Doty
patent: 6161062 (2000-12-01), Sicre et al.
patent: 6782742 (2004-08-01), Adebjork et al.
patent: WO97/26553 (1997-07-01), None

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