Tytuł pozycji:
Active control of vibrations of gyroscope on rocket deck
The paper discusses errore of astatic gyroscope, located on board of a homing missile, suspended on Cardan joint. The impact of friction in suspension bearings, the base kinematic input and linear accelerations on the gyroscope axis position are also investigated. The paper gives the algorithm for the optimum correction control. Its role is to minimise the impact of rocket vibrations and manoeuvres on the gyroscope work accuracy.