FIELD: inertial control system. SUBSTANCE: method can also be used in manufacture of precision gyroscopes. Speed of own rotation of rotor is changed with excited nutational vibrations. Nutational frequencies are measured with two values of speed of rotor and slope is calculated as difference between ratio of increment of frequency of nutational vibrations to increment of speed of own rotation of rotor and one. EFFECT: improved authenticity of method. 1 dwg
Authors
Dates
1996-06-27—Published
1983-11-21—Filed