FIELD: determination of flying and navigational parameters of flying vehicles.
SUBSTANCE: proposed method includes formation of inertial navigational multi-system including two navigational computers with two sets of meters, swivel unit for turning the meter sets and modulating the vector of error of present orientation of coordinate measuring system. Proposed system ensures measurement of error vectors, bringing of error difference modulus to maximum magnitude for compensation of entire present orientation error vector of coordinate measuring system with all components in space taken into account.
EFFECT: enhanced accuracy of determination of flying vehicle navigational parameters.
3 cl, 1 dwg
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