FIELD: armament, in particular, rocketry, applicable in development of rocket complexes, where flight vehicles are used as a carrier, as well in development of complexes on the ground, in which, for example, beam tele-guidance systems are used.
SUBSTANCE: offered is the method for formation of rocket control commands at which formed commands to the rocket are fed from control station, and the control commands are received and produced on the rocket. Additionally, on the launcher in compliance with rocket orientation in the bank angle, switching of contacts are preset, which form a binary number, memorized it and with due account of the value of the binary number, the value of the initial phase of the rocket control commands is formed, which has expanded the field of application due to installation of the rockets on various carriers at variation of modifications of rocket suspensions to the launcher. Described is the rocket complex having a rocket, comprising the members of the rocket electromechanical joining, unit of reception and processing of control commands and a power drive. The members of the electromechanical joining of the rocket are coupled with the electric power supply system of the control station via a device of the electromechanical joining of the launcher and the electromechanical circuits of rocket launching preparation. Introduction in the rocket complex on the rocket of the write signal driver and series connected binary number driver, storage, phase shifter, and a switch on the launcher that is coupled to the input of the binary number via the device of the electromechanical joining of the launcher and components of the rocket electromechanical joining, has expanded the field of application due variation of the rocket suspensions from the launcher obtained by the respective turning of the rocket in bank angle on the launcher at variation of the initial phasing.
EFFECT: expanded field of application.
3 cl, 2 dwg
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