FIELD: military equipment.
SUBSTANCE: invention relates to military equipment and can be used in jet valley fire systems (MARS). Method comprises guiding launcher (L) in horizontal plane in direction of target, lifting guides with rocket missiles (RS) through preset angle starting in vertical plane (VP), estimating time (WS) of flight in system of independent flight path correction (SAKT) PC at initial section of path, including solid rocket engine start is PC at small angle in the IP at initial section of flight trajectory (UTV) PC taking into account technical characteristics of PU and relief arrangement PU, PC is transferred to a new path with large angle in VP after expiry of WS considering conditions of non-detection PC at initial section of trajectory of radar station counter-battery control (CBS) of enemy PC is launched with subsequent according to preset flight ballistic trajectory, simulating start of PC of fictitious point spaced from LS at a safe distance, excluding damage PU enemy artillery fire by results of locating radar station CBS start position MARS controlled pitch and yaw angles PC with help of gas-dynamic rudders by commands from SAKT PC depending on safe flight altitude of PC, which prevents detection by radar CBS, removal of PU from radar station from front line, minimum angle of view of radar station CBS branch of apparent start angle, angle of start PC branch PC speed vector angle corrections to angle of start PC, PC flight speed, permissible overload PC branch of free fall acceleration, hit target.
EFFECT: higher efficiency of firing MARS.
1 cl, 2 dwg
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Authors
Dates
2016-11-10—Published
2014-12-29—Filed