FIELD: equipment for satellite inertial navigational and gyrostabilization systems for sea-going objects.
SUBSTANCE: proposed inertial navigational systems uses information from gyroscopes and accelerometers for autonomous generation of navigational and dynamic parameters of motion of sea-going objects and correcting information of satellite navigational system pertaining to coordinates of object position. In case of complicated situation of operation of satellite system when orbital cluster of spacecraft is reduced, use is made of stand-by mode of correction of inertial system according to the data of primary measurement. Correction signals are generated on basis of external information data and navigational data, thus enhancing accuracy of navigational determination under standard conditions of functioning.
EFFECT: enhanced accuracy of determination.
3 dwg
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