FIELD: airborne armament. SUBSTANCE: proposed group of inventions is related to armament means of wide class of military aircraft and helicopters. Practice of control over armament is based on detection of target, determination of its parameters, selection of weapon, formation of control signals by scanning sighting means and weapons. Apart from it mode of operation of armament control system is specified, master channel of armament control system is selected and operation conditions of scanning sighting means and weapons are formed in correspondence with them. Armament control system incorporates weapon control system intercoupled with aircraft rocket homing aids, connected to indication system, radar, optic location station. Above-mentioned stations include control computers. In addition armament control system is equipped with target indication former for aircraft rocket homing aids which switches over target indication depending on operation conditions of weapons and with switch changing modes of operation of armament control system. All specified elements of system are properly intercoupled to execute control over armament. Control computer of radar demonstrates potential for formation of sign of master channel of armament control system depending on selected weapon, mode of operation of armament control system and conditions of location aids, on formation of operation conditions of radar, weapon and indication system as well as on identification of targets. Computer of optic location station can form modes of operation of optic location station and target identification. EFFECT: given design makes it feasible to use completely potential of armament means and crew, to raise probability of carrying out combat task under various tactical conditions and interference situations. 12 cl, 4 dwg, 3 tbl
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Authors
Dates
2003-06-10—Published
2001-12-04—Filed