Magnetic flux detector correction system

G - Physics – 01 – C

Patent

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324/48

G01C 17/38 (2006.01)

Patent

CA 1239990

ABSTRACT OF THE DISCLOSURE An aircraft heading correction system utilizing the horizontal field strength of the earth's magnetic field to determine the tangent of the dip angle generally associated with a given field strength. The tangent of the dip angle is then used to generate a signal which corrects the flux valve heading during accelerated flight.

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