FIELD: physics.
SUBSTANCE: method comprises initial alignment of a gyrostabilised platform; determining orientation of the coordinate system associated with the gyrostabilised platform relative to the local horizontal coordinate system associated with the Earth; calculating the result of independent determination of the azimuth of the gyrostabilised platform αη; determining the astronomical azimuth ACE of the control element of the gyrostabilised platform, the position of the normal to which coincides with the zero reading of an angle φ sensor; at the end of the initial alignment, measuring the angle φ of the gyrostabilised platform around the axis of a gimbal suspension and determining the gyrocompassing error ΔA: ΔA=αη-ACE-φ; alignment of the gyrostabilised platform is considered to have passed the inspection of the gyrocompassing error does not exceed an acceptable value.
EFFECT: high reliability of inspecting initial alignment of a gyrostabilised platform.
3 dwg
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Authors
Dates
2015-02-10—Published
2013-10-03—Filed