METHOD OF INTRODUCING ROCKETS INTO ZONE OF CONTROL, ROTATING ALONG ANGLE OF LIST, AND ROCKET SYSTEMS Russian patent published in 2009 - IPC F41G7/00 F41F3/04 F42B15/00 

FIELD: aviation.

SUBSTANCE: invention belongs to the field of armaments, and specifically to rocket technology and can be used in rocket systems with rockets rotating along the angle of the list on flight trajectory. The method is suggested for the introduction into the zone of control of the rocket rotating along the angle of list, during which, up to the moment of the initial formation of the linearised, alternating signal, exposes the size of the transforming and linearised signals which are constant and distinct from each other, which form the maximum relay value for control commands by pitch according to the declination of the rocket above. After the initial formation of the linearised signal they present the values of the deciphered signal for course and pitch equal to zero until the moment of the rocket's introduction into the zone of control. The introduction of the rocket system onto the rocket timer and in turn the unification of devices for turning on the onboard energy source, memory driver for the non-recurrent signal and the lock engine for initial commands exclude errors at the moment of initial formation for command control.

EFFECT: elimination of errors at the at the moment of initial formation for command control, which enables the reduction of values for minimal sighting range.

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