COMBINED NAVIGATIONAL COMPLEX OF FLYING VEHICLE

FIELD: navigational complexes of flying vehicles, multi-mission fighters and helicopters in particular. SUBSTANCE: proposed combined navigational complex includes inertial navigational system, satellite navigational system, navigation computer, navigation information recorder, inertial navigational...

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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: navigational complexes of flying vehicles, multi-mission fighters and helicopters in particular. SUBSTANCE: proposed combined navigational complex includes inertial navigational system, satellite navigational system, navigation computer, navigation information recorder, inertial navigational system error computer, energy-independent storage and first computer of errors to speed components and azimuth angle of gyro-platform of inertial navigational system. Introduced additionally are flying vehicle speed single-beam radar meter, speed radar meter error computer and second computer of errors to speed components and azimuth angle of gyro-platform of inertial navigational system. EFFECT: enhanced accuracy of determination of navigational parameters, noise immunity and resistance to failure. 1 dwg