G - Physics – 06 – F
Patent
G - Physics
06
F
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.
370644
Evans James D.
Pool Sam L.
George H. Riches And Associates
Hydac Inc.
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