COMBINED NAVIGATION SYSTEM

FIELD: navigation, navigation complexes of aircraft, predominantly, multipurpose fighters and helicopters. SUBSTANCE: combined navigation system incorporates attitude-and-heading reference system, system of air signals, computer of components of wind velocity, storage, navigation computer, integrato...

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Bibliographische Detailangaben
Hauptverfasser:	STAROVEROV A.CH, VOLKOV G.I, IL'IN V.V, MASLENNIKOV V.G, KORZHUEV M.V, VAVILOVA N.B
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	GYROSCOPIC INSTRUMENTS MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS SURVEYING TESTING
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Beschreibung
Zusammenfassung:	FIELD: navigation, navigation complexes of aircraft, predominantly, multipurpose fighters and helicopters. SUBSTANCE: combined navigation system incorporates attitude-and-heading reference system, system of air signals, computer of components of wind velocity, storage, navigation computer, integrator of components of velocity and radar velocity meter determining projection of velocity of aircraft on direction of its beam while it scans and generating data on direction of scanning beam in azimuth and with reference to plane of horizon. EFFECT: enhanced precision of computation of coordinates of aircraft. 3 dwg