FIELD: military equipment.
SUBSTANCE: invention refers to antiaircraft weapons system of short-range and is aimed to hit air, mainly low-flying, targets. The transport means (1) has double-coordinate turn device (2) with a unit (3) of anti-aircraft missiles with homing heads (4) with optic-electron channels (18). Antiaircraft weapons system includes also optic-electron system with target head (7), installed at the unit (3) of anti-aircraft missiles, calculation unit (8), monitor (9) and control unit (10). There is also a unit (17) of image alignment the inputs of which are connected electrically to outlets of optic-electron channels (18) of homing heads (4) and the output is connected electrically to the input of calculation unit (8). Photodetectors (20) of optic-electron channels (18) of homing heads (4) are of matrix type. Dimensions of objectives (19) fields of view of homing heads (4) optic-electron channels (18) are made so that in certain orientation in space these objectives (19) could have possibility to jointly lap the space under review with no gaps creating together a wide field of view equal in dimensions to objective (14) field of view of optic-electron system target head (7). The unit of image alignment (17) is made so that it is possible to receive separate narrow-field images of joint wide-field image of viewed space of optic-electron channels (18) of homing heads (4) equal to wide-field image of target head (7) of optic-electron system.
EFFECT: antiaircraft weapons system is characterized by increased effectiveness due to the possibility to rocket firing of several targets.
5 cl, 2 dwg
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Authors
Dates
2012-02-20—Published
2010-06-23—Filed