FIELD: navigation. SUBSTANCE: values of atmospheric pressure are measured at flight altitude of flying vehicle and at sea level, temperature at sea level 15 measured and temperature gradient of change of air temperature is taken, current values of air temperature at airfield and airfield altitude above sea level are determined and flight altitude of flying vehicle is calculated. EFFECT: improved authenticity of determination of flight altitudes. 2 cl, 1 dwg, 1 tbl
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Authors
Dates
1995-10-27—Published
1992-08-10—Filed