FIELD: flight vehicle control systems, in particular, beam systems of rocket TV guidance, applicable for fighting against enemy military equipment.
SUBSTANCE: according to the method, a spinning signal is formed on the rocket. Then, the received control signals are decoded, and control commands are produced. The moment of appearance of the spinning signal is registered, the beginning of the time count is specified by it, during which the parameters of the rocket control equipment are changed, and the correction of the rocket control commands is effected. The rocket has a gyroscopic roll sensor, control actuator and series-connected receiving channel and a coordinate converter, whose control input is connected to the output of the gyroscopic roll sensor. The rocket has also a retainer and a former of the changed commands. The retainer input is connected to the output of the gyroscopic roll sensor. The retainer output is connected to the control input of the former of the changed commands, whose signal input is connected to the output of the coordinate converter, and the output - to the input of the control actuator.
EFFECT: enhanced accuracy of rocket guidance to the target.
2 cl, 1 dwg
