FIELD: weapons.
SUBSTANCE: invention relates to weapons, in particular to missile systems. Missile system comprises a launcher with a guidance system in horizontal and vertical planes, a field computer with an autonomous power source, automation unit with independent power supply, navigation satellite receiver, means of orientation in horizontal and vertical planes, as well as in roll and pitch. Output of the navigation satellite receiver is connected to the input of the field computer, the input of the automation unit is connected to the output of the field computer, and the output of the automation unit is connected to a switching connector for connecting the transport-launching container of the missile. Automation unit incorporates a control module, a controlled power supply system, and a sensor for the presence of a missile launching container. Navigation satellite receiver is in form of a sensor of data on initial digital navigation information, which includes data on system time, on ephemerides and almanacs on spacecraft of a satellite navigation system.
EFFECT: ensuring the possibility of hitting a target located outside the line of sight of the complex from closed firing positions.
5 cl, 1 dwg
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