A GUIDANCE SYSTEM FOR A SHORT-RANGE ANTI-AIRCRAFT MISSILE UNIT

1. A guidance system for a short-range anti-aircraft missile unit, comprising mounted on a single self-propelled carrier, or in a conveyance container, detection means 2 having an all-round looking radar; radar-based identification interrogator 4; means 10 for tracking and precision-measurement of the target and missile coordinates; means 22 for displaying an information; devices 6 for the missile pre-launch preparation and launch execution; transponder 18; missile autopilot 19; computation control means, including evaluator 7 for evaluating the time a target enters the launch area, and evaluator 14 for evaluating the angle misalignment, characterized in further comprising: means 1 for partial controlling of antenna beams of the all-round looking radar, having a phase-shift device; means 3 for the range and azimuth tracking; system 8 for controlling the beam of a radar of means 10 for tracking and precision-measurement of coordinates, the antenna of which radar is implemented in the form of a phased array; programmable search device 9; system 11 for simultaneous tracking basing on four coordinates (azimuth, elevation, range and Doppler frequency) of a number of objects using the radar of means 10 for tracking and precision-measurement of coordinates; device 17 for controlling the pattern width; missile beacon 21; tracking radar 20 of missile beacon 21; switching device 15; device 13 for identification of the target class and adapting the modes of operation of the missile control systems, including a signal spectral analysis unit; evaluator 16 for evaluating the pre-launch command information and missile deviation angles after the vertical launch; device 12 for analysing the launch results; and the computation control means further comprises second evaluator 5 for evaluating the time a target enters the launch area; the pattern of antenna of radar-based identification interrogator 4 being deployed in azimuth relative to the antenna of the all-round looking radar of detection means 2 in the direction opposite to that of rotation of the latter; a transmitter of the all-round looking radar of detection means 2 being connected to the phase-shift device of means 1 for controlling the antenna beams of the all-round looking radar of detection means 2, which phase-shift device is connected to antenna emitters of the all-round looking radar of detection means 2; output of a receiving system of the all-round looking radar of detection means 2, which system is of the