METHOD OF DETERMINATION OF FLIGHT ALTITUDE OF FLYING VEHICLE Russian patent published in 1995 - IPC

Abstract RU 2040443 C1

FIELD: aeronautical engineering. SUBSTANCE: parameters of flow near flying vehicle are measured and aerodynamic parameter which changes under action of screen is formed. Parameters of flow, motion and configuration of flying vehicle are determined. Flight altitude is determined from calibration relationship from indicated parameters formed in flight experiment. EFFECT: enhanced efficiency. 3 cl, 3 dwg

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RU 2 040 443 C1

Authors

Pushkov S.G.

Sokoljanskij V.P.

Vdovin O.K.

Panatov G.S.

Dolbnja L.A.

Filippov B.V.

Goncharov I.I.

Dates

1995-07-25Published

1992-03-24Filed