COMBINED NAVIGATIONAL COMPLEX OF FLYING VEHICLE Russian patent published in 2004 - IPC

Abstract RU 2224220 C1

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

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RU 2 224 220 C1

Authors

Vavilova N.B.

Volkov G.I.

Il'In V.V.

Korzhuev M.V.

Maslennikov V.G.

Staroverov A.Ch.

Dates

2004-02-20Published

2003-03-24Filed