CONTROL SYSTEM FOR SELF-GUIDED MISSILE Russian patent published in 2005 - IPC

FIELD: air defense.

SUBSTANCE: system comprises housing connected with four return springs each of which is connected with the corresponding air vane, propulsion engine, four photomultiplier tubes of the guidance system which are connected in the arms of the electric bridge, four air vanes connected with the electromagnets with movable core through intermediate relay, four infrared devices for photomultiplier tubes, four vision limiters for photomultiplier tubes, four DC amplifiers for photomultiplier tubes, board power source, four tail stabilizing fins, analogue-digital converter, and control unit composed of integrator, tree-link integrating device, and inverter. The photomultiplier tubes are connected with the analogue-pulse converter, intermediate relay, integrator, inverter, and three-link integrating device through the DC amplifier.

EFFECT: accelerated missile aiming.

7 dwg