FIELD: measurement equipment.
SUBSTANCE: they carry out the compensation of errors of a unit of accelerometers due to errors of accelerometers of the second unit by the rotation of sensitive elements to the achievement of the maximum of difference of the readings of the accelerometers reduced to a single system of coordinates. The device is an inertial navigation multi-system, which comprises two navigation calculators, two units of gyroscopes, two units of accelerometers and a system of control of the spatial position of units of sensitive elements.
EFFECT: increased accuracy of detection of pilot and navigation parameters of the aircraft flight.
3 cl, 1 dwg
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