METHOD OF GENERATING CONTROL INSTRUCTIONS AT MISSILE SPINNING IN ROLL ANGLE AND SYSTEM TO THIS END, METHOD OF SELECTING SET PULSES AT MISSILE REVOLVING IN ROLL ANGLE AND DEVICE TO THIS EFFECT, AND METHOD OF DEFINING MISSILE ROLL ANGLE Russian patent published in 2013 - IPC F41G7/00 

FIELD: weapons and ammunition.

SUBSTANCE: count pulses are generated on the basis of logical addition of two identical trains of pulses shifted through 90° relative to each other and generated at roll transducer outputs after launching. Note here that said local addition results in generation of two pulses. First pulse corresponds to missile roll angle equal to zero while second pulse equals 90°. First or second pulse is selected to reset missile control system. Versions of said system incorporate functional units to generate missile adaptive control effects.

EFFECT: higher accuracy.

7 cl, 3 dwg