FIELD: control system.
SUBSTANCE: the missile self-destroying device has a condition multiplexing unit, control unit, the first and second power supply sources, the first and second trajectory sensors, control bus-bar, input bus-bar, the first and second electric detonators. The control input of the condition multiplexing unit is connected to the control bus-bar, and its first input is connected to the first power supply source via the trajectory sensor. The second input of the condition multiplexing unit is connected to the output of the control unit, whose input is connected to the output of the second power supply source, and the control input-to the input bus-bar. The second output of the condition multiplexing unit is connected to the input of the second electric detonator, and the input of the first electric detonator is connected via the trajectory sensor to the first output of the condition multiplexing unit.
EFFECT: provided self-destroying of the missile at a non-standard launch of it.
1 dwg
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