METHOD OF FIRING GUIDED MISSILE WITH LASER SEMI-ACTIVE HOMING HEAD

FIELD: weapons and ammunition.SUBSTANCE: invention relates to control artillery guided projectiles and missiles with laser semi-active homing head (HH), exciting is illuminated with target at final path, and is intended for control of mortar and cannon of 120, 122, 152, 155 mm gauges in fire by guided munitions, as well as guided missiles with homing heads. Said task is achieved by using installation target designator to drone (UAV) to target auto tracking, detection and further automatic tracking by target designator. There is possibility of determining speed of unmanned aerial vehicle, topographic referencing target designator, fire position and target and periodically transmission with frequency of 0.2 to 5 Hz coordinates and speed of target designator to fire position, measurement of polar coordinates of target relative to target designator, transmission of digital radio communication on fire position, calculating firing settings in it and their implementation, installation of single computer time in director and on fire position , working on fire position resolution on shot and its production, besides, it is formed after checking ingress of laser radiation reflected from target designator in field of view of guided missile homing head at approach to target, transmission with fire position on pointer along channel of digital radio communication time of laser radiation and its connection when required, homing of projectile on target, is illuminated with laser target designator.EFFECT: higher safety of target designator, faster solving tasks of survey and shooting control, expanded applications of controlled artillery ammunition with laser semi-active homing head due to arrangement of target designator at UAV.3 cl Изобретение относится к управлению артиллерийскими управляемыми снарядами и ракетами с лазерной полуактивной головкой самонаведения (ГСН), захватывающей подсвеченную цель на конечном участке траектории, и предназначено для управления огнем минометов и ствольной артиллерии калибров 120, 122, 152, 155 мм при стрельбе управляемыми боеприпасами, а также управляемыми ракетами с ГСН. Указанная задача достигается использованием установки целеуказателя на беспилотном летательном аппарате (БЛА) с возможностью автосопровождения цели, ее обнаружения и дальнейшего автоматического сопровождения целеуказателем. Имеется возможность определения скорости движения БЛА, топографической привязки целеуказателя, огневой позиции и цели к местности и передачи периодич