METHOD FOR MISSILE FIRING AND MISSILE GUIDANCE SYSTEM Russian patent published in 2003 - IPC

FIELD: optical guidance systems of self-propelled projectiles, applicable in systems of guided weapon with teleorientation in the laser beam. SUBSTANCE: adjustment of the axes of all the launchers included in the control system with its optical axis is preliminarily conducted. The conditions of firing are preset, one of the launchers for firing is assigned, a command is given to put the control system in the condition corresponding to the firing condition, and then the condition of the control system is checked. After the above check a permission or prohibition for firing is given. In case of a prohibition for firing is given. In case of a prohibition the mentioned system is brought to a condition satisfying the conditions of firing, or another launcher is assigned for firing, after that the condition of the control system is checked again. The missile guidance system additionally as a range-finding channel, logic unit, reset button, pancreatic optical system reset unit, radiation sensor, modulator rotational speed transducer and a position pick-up of the pancreatic optical system, excess introduction device, as well as a position pick-up of the excess introduction device. EFFECT: provided guidance of missiles of different types with guarantee of their error performance and automated process of their launching. 7 cl, 3 dwg