CONTROL METHOD OF EQUIPMENT OF AIR DEFENSE ROCKET-CANNON COMPLEX

FIELD: weapons and ammunition.SUBSTANCE: invention refers to control of equipment of air defense rocket-cannon complexes. The control method of equipment of the air defense rocket-cannon complex involves detection and identification of a target, taking of firing decision and calculation of coordinat...

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Hauptverfasser: CHERKASOV VLADISLAV NIKOLAEVICH, CHEKINOV SERGEJ GENNAD'EVICH, BYT'EV ALEKSEJ VJACHESLAVOVICH, TKACHENKO VLADIMIR IVANOVICH, KUPRIJANOV GENNADIJ PAVLOVICH
Format: Patent
Sprache:eng ; rus
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Zusammenfassung:FIELD: weapons and ammunition.SUBSTANCE: invention refers to control of equipment of air defense rocket-cannon complexes. The control method of equipment of the air defense rocket-cannon complex involves detection and identification of a target, taking of firing decision and calculation of coordinates of a predicted collision point for firing by means of rocket and cannon equipment, guidance of equipment and rocket and/or shell firing, evaluation of firing results and taking decisions on firing continuation. At rocket firing, an aiming mark is aligned with the target by means of a sight; an air flow velocity is measured; angular corrections for deviation both of rocket and cannon equipment from a sighting line are determined considering firing conditions and ballistic characteristics of ejected rockets and shells, availability in the sight field of view of dust and smoke interference and their characteristics; the above corrections are entered to guidance actuators of the corresponding equipment; during flight of the guided rocket and after it is captured with a guidance system, in a number of the trajectory sections there performed is its deviation from the sighting line by correction of control commands of input of an additional constant signal and pseudorandom signals of a random number generator; besides, maximum level of corrected control commands and a deviation value of the rocket from the sighting line are restricted in a perspective plane perpendicular to the sighting line, and when the rocket approaches the target at the specified distance, correction of rocket control commands is stopped.EFFECT: improving probability of target hitting and reducing probability of hitting of the guided rocket itself. Изобретение относится к области управления вооружением зенитных ракетно-пушечных комплексов. В способе управления вооружением зенитного ракетно-пушечного комплекса осуществляют обнаружение и опознавание цели, принятие решения на стрельбу и вычисление координат упрежденной точки для стрельбы ракетным и пушечным вооружением, наведение вооружения и стрельбу ракетой и/или снарядами, оценку результатов стрельбы и принятие решения на продолжение стрельбы. При стрельбе ракетой с помощью оптического прицела совмещают прицельную марку с целью, измеряют скорость воздушного потока, определяют угловые поправки на отклонение и ракетного, и пушечного вооружения от линии прицеливания с учетом условий стрельбы и баллистических характеристик выстреливаемых ракет и сна