FIELD: weapons and ammunition.
SUBSTANCE: group of inventions relates to a method and a system for controlling the flight of rocket missiles (RM). To control the RM flight, the launcher is directed towards a group of targets based on data from the radar station, each projectile is numbered when it is installed on the guide frame to determine the time of transmitting the command for its launch, as well as launching other RMs (four pieces at a time), trajectories of RM and mobile targets are determined, a correction signal is generated depending on the range to the target and the approach speed, correcting pulse values are selected based on stability criterion and transmitted to each numbered RM. System comprises ground equipment as part of a command post, a radio transmitter, a radar station, an electronic computer, a launching device, four RM, situation evaluation unit and onboard equipment arranged on missiles, comprising: a receiving device, a counter, four AND logic elements, four solenoids, four blades providing projectile control in horizontal and vertical planes.
EFFECT: higher accuracy of firing of rocket missiles.
3 cl, 6 dwg
