METHOD FOR ROCKET CONTROL AND ROCKET GUIDANCE SYSTEM FOR ITS REALIZATION Russian patent published in 2007 - IPC F41G7/24 F42B15/01 

FIELD: armament, in particular, rocketry, may be applicable in development of missile complexes, for example, with carriers on the ground in which ray television systems are used.

SUBSTANCE: the method is based on the fact the control signal is limited unilaterally excluding from it the values of the quantities corresponding to the downward direction of the control signal, from the moment of rocket take-off the current time is measured, and a pulse signal is produced at the preset time moment, which assigns the formation of the pitch control command at first by the control signal and then by a limited control signal up the end of the flight. The offered locket guidance system uses a timer and a switched-over limiter, the timer output is connected to the first input of the switched-over limiter, whose second input is connected to the adder output, and the output of the switched-over limiter is connected to the input of the pitch autopilot.

EFFECT: enhanced efficiency due to prevention of rocket fall.

2 cl, 3 dwg