An arrangement for, in particular mobile, flight defence systems

摘要

Fire control device, in particular for mobile, flight defence systems with an about a vertical axis (11) rotatable platform (10), with at least one on the platform (10) arranged, about a horizontal axis (14) pivotable weapon (12, 13) for a guided missile equipped with homing head, with at least one with the weapon (12, 13), rigidly coupled, optical target tracking sensor (25), which in the case of the target aligned line of sight (31, 32) is continuously target data, such as destination position, speed, target distance, determined, with a with the target tracking sensor (25) is connected to the directional angle computer (42), which consists of the target data the expected meeting point of guided missile and aerial target, as well as the required directional angle "aiming-off allowance or offset and" paper "of the guided missile for the firing is calculated, with a with the target tracking sensor (25) of the linkage means 17-20 could be connected to computer (41), which consists of deviations of the target position of the line of sight (31) of the target tracking sensor (25) as claimed in the azimuth and elevation signals of the linkage means 17-20 could be produced, and with a with the tracking - and directional angle computer (41, 42) control unit (46) connected with actuating drives (22, 23) for platform (10) and weapon (12, 13), the..