FIELD: military equipment.
SUBSTANCE: invention relates to defense equipment and can be used in guided weapon systems for hitting fixed targets located in depth of battle formations of enemy. High-precision weapon guidance system, comprising ground equipment for radiotelemetric control of command station and air target designation system, includes a microprocessor situation optimiser connected with equipment located on rocket. Before start, situation optimiser is connected to first input of control command decoder. After start-up at initial and intermediate sections of trajectory, communication is carried out in radio remote control mode - via radio channel with radio receiver and radio transponder of missile. Output of radio receiver is connected to second input of control command decoder, first output of which is connected to first input of command switch, its output is connected to control equipment, its first output is connected to input of steering drive, and second output is connected to input of radio transponder. Missile includes a self-contained line simulator consisting of a self-contained time generator, altitude simulator. Vernier simulator, trajectory controller. Second output of control command decoder is connected to input of self-contained time generator. Output of self-contained time generator is connected to input of altitude simulator, output of which is connected to input of vernier simulator, its output is connected to first input of trajectory controller, second input is connected to output of self-contained time generator. Output of trajectory controller is connected to second input command switch, third input of which is connected to output of self-contained time generator.
EFFECT: improved tactical capabilities of ground equipment for radiotelemetric control of command station and elimination of effect of active interference at transition of missile into autonomous mode of approach to target.
1 cl, 1 dwg
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