METHOD FOR CONTROL OF MISSILE TAKE-OFF AND MISSILE COMPLEX Russian patent published in 2007 - IPC F42B15/00 F41F3/04 

FIELD: armament, in particular, rocketry, applicable in development of guided armament complexes.

SUBSTANCE: the energy generated at the launcher is fed to the missile, where it is converted to an electric signal that accomplishes the control of the missile take-off, the pretake-off setting and starting of the roll-angle pick-off inclusive. The missile complex has: on the missile-an adjustable roll-angle pick-off and an energy converter, and on the launcher-an energy generator that is coupled to input of the energy converter and to the electric power supply source. The output of the energy converter is connected to the starting inputs of the on-board power supply source, adjustable roll-angle pick-off and the launcher starting device. The outputs of the adjustable roll-angle pick-off and the pitch-angle pick-off are connected to the respective inputs of the on-board control equipment.

EFFECT: enhanced reliability and to the exlusion of electromechanical linkage between the missile and the launcher.

2 cl, 1 dwg