Digital altimeter computer

G - Physics – 06 – F

Patent

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73/168, 354/25

G06F 15/20 (1980.01)

Patent

CA 1156759

ABSTRACT A new and improved computing apparatus for determining aircraft altitude has a pressure transducer to sense atmospheric pressure at which the aircraft is located, and from this and a preset local ground level atmospheric pressure reading, actually solve a non-linear altitude- pressure equation. The computed altitude is used in con- junction with a time measurement to determine aircraft vertical rate. The computed altitude also specifies an address in a memory circuit, with the data stored at such address being the grey code which is transmitted to others for air traffic control purposes.

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