A method for measuring combined index system of satellite hemispherical resonator gyroscope
A hemispherical resonant gyroscope and measurement method technology, applied in the field of satellite attitude control, can solve the problems of measuring the combined deviation of satellite gyroscopes and inapplicability of measurement methods, and achieve the effects of avoiding calculation, improving measurement accuracy and improving attitude control accuracy.
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[0022] The method steps of the present invention will be further described below in conjunction with the drawings and embodiments.
[0023] Step 1, use the reference plane to flip the tooling to measure a single gyroscope
[0024] Such as figure 1 As shown, it is a schematic diagram of the reference plane turning tool used in the present invention,
[0025] Taking the bottom surface of the reference plane flipping tool as a reference, the gyroscope assembly with three orthogonal and one inclined gyroscopes is installed on the slope 22 of the reference plane flipping tool, so that a single gyro installed on the slope 22 is in a vertical state with the horizontal plane;
[0026] Step 2, measure the performance index of a single gyroscope
[0027] 1) The axis of the single gyro to be tested must be perpendicular to the horizontal plane;
[0028] 2) Measure the performance index of a single gyroscope installed on an inclined plane;
[0029] 3) Flip the datum plane Flip the two...
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