GUIDED MISSILE Russian patent published in 1999 - IPC

FIELD: missile weaponry. SUBSTANCE: missile body accommodates the electronic control equipment, electric power unit, control actuator and a gyroscope with a contactless sensor. The gyroscope and control actuator are rigidly fastened to the surfaces of common support coupled to the missile body. The control actuator is supported as a cantilever with respect to the support, and with a clearance with respect to the missile body, and its fasteners are located around the gyroscope and points of its attachment to the support. EFFECT: enhanced accuracy and reliability of guided missile attained due to linearization of friction moments in gyroscope ball bearing supports due to the effect of vibrations arising in operation of the control actuator. 2 dwg