FIELD: missile technology, in particular to the field of automatic control of non-rotating missiles with aerodynamic control.
SUBSTANCE: missile contains a satellite navigation system made in the form of a four-channel receiver, an adaptive robust filter, a software super-narrow correlator, a NeuroMatrix series processor. At least four satellite navigation system receiver antennas are installed on board the missile. The satellite navigation system receiver contains 40 tracking channels for navigation spacecraft of GPS, GLONASS, GALILEO satellite navigation systems. By means of the receiver of the navigation system, the values of the deviation of the vertical line of the missile are determined and when these values go beyond the specified limits, they decide on the self-destruction of the missile.
EFFECT: present invention enables to increase the efficiency and safety of the use of missiles in case of emergencies on board the missile during testing and in combat conditions.
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