A variant of an automatic safety control system provided firing with guided missiles on a ground with limited extent is considered. The system implies using radar information received by a spaced multiposition active-passive detection system. Information about aerodynamic targets is received by means of using the radar field, present at the ground, and a radar situation analysis algorithm. As a result of the analysis decisions on the guided missiles firing safety degree and the missile secure neutralization in case of worst-case situation are made.
radio-location station, multiposition radio-location system, exposure of aims, measuring of co-ordinates, determination of complete vector of speed of aerodynamic aims, control, after motion of target and zenithal guided rocket, decision-making about a degree safety of leadthrough of the rocket firing