FIELD: military equipment.
SUBSTANCE: invention relates to the field of military equipment and relates to a method for guiding a missile. The method includes tracking the target and determining its coordinates with a thermal imaging system relative to the center of the thermal imaging raster, launching the rocket and counting the current time t from the moment of its descent, capturing, tracking and measuring the coordinates of the rocket with the thermal imaging system relative to the center of the thermal imaging raster, determining the deviation of the rocket from the target, generating and the transmission of control commands to the missile. The rocket is captured by the thermal imaging system every time the rocket appears within the thermal imaging raster, and the tracking and measurement of the rocket coordinates by the thermal imaging system is always performed when the rocket is present within the thermal imaging raster.
EFFECT: technical result consists in increasing the accuracy of the missile guidance.
4 cl, 1 dwg
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Authors
Dates
2021-03-30—Published
2020-06-05—Filed