Mathematical model of instrumental vibration error of angular velocity sensor

The problem of mathematical description the influence harmful deterministic and broadband random vibrations a moving object on measurement result sensor angular velocity rotation this installed it is considered. It shown that under such conditions systematic instrumental vibration error arises in sensor. source nonlinearity static conversion function asymmetry its coefficient.
 A model has been obtained. Formulas for calculating vibrational are obtained depending apparent flight aircraft, parameters base which nonlinear function.
 This makes possible to calculate value specified specific (direct analysis problem), as well select an based values ​​of coefficients, ensuring required accuracy measuring using (inverse synthesis problem).