FIELD: instrument engineering, in particular, navigation instruments for determination of the main navigational parameters of positioning of air an ground objects.
SUBSTANCE: the control signals of the gyroplatform or gyroplatform model are formed proceeding from the condition of provision of natural period of vibrations of gyroplatform or gyroplatform model at an absence of ballistic deviation as distinguished from the Shuller period. The asymptotic stability (independent damping) of each inertial system or inertial system model is provided.
EFFECT: enhanced accuracy due to expansion of the dynamic measurement range of the gyroscopic vertical.
4 cl, 4 dwg
