| 摘要 |
FIELD: weapons and ammunition.SUBSTANCE: guided missile in transporter-launcher container comprises an accelerating engine, a main engine, a combat unit, a steering compartment and an onboard connector. The steering compartment comprises a secondary power source, a unit of formation of a single-channel control signal and a steering machine connected to it, as well as the instrumental part with elements of radio command control system in the form of a radio receiving unit and unit of responder. The onboard control system of the missile is made dual-system through the introduction in the instrumental part of a photodetector of the laser-beam control system, the system control unit, the control module, the unit of equivalent load, the power supply. The output of the secondary power source is connected to the second input of the unit of responder and the first input of the unit of the equivalent load. The output of the control module is connected to the second input of the unit of the equivalent load, the third input of which is connected to the contact of the carrier onboard connector designed for automatic selection and commutation of elements of one of the said control systems of the missile for operation in accordance with the control system of the carrier.EFFECT: expansion of combat capabilities of the missile.4 cl, 8 dwg |
