FIELD: defense equipment, in particular, mobile antiaircraft complexes, applicable for organization of antiaircraft defense of troops and military objects against destruction by enemy means of air attack. SUBSTANCE: the self- propelled antiaircraft rocket mount has a phased aerial array, radar station, rotatable launcher with rockets and transducer of the angle of rotation, digital computer, gyroscopic system of measurement of the heading, bank and pitch angles, as well as the navigation, topographic survey and orientation system, use is also made of the system of comparison and storage of the angles of the gyroscopic system and the system of correction of time instability of the gyroscopic system of angles measurement. The output of the gyroscopic system is connected to the combined inputs of the system of comparison and storage and the system of time instability of the gyroscopic system. The navigation, topographic survey and orientation system is coupled respectively to the input of the gyroscopic system and to the second input of the comparison and storage system, the transducer of the rotary angle of the launcher is connected to the third input of the comparison and storage system, whose output via the system of correction of time instability of the gyroscopic system is connected to the central computer, whose output busbar is coupled to the phased aerial array. EFFECT: the self-propelled mount for detection, tracking, guidance and launching of rockets of the medium-range antiaircraft rocket complex provides for prolonged combat operation simultaneously against several perspective means of air attack, first of all against winged missiles flying at extreme low altitudes due to elimination of the time instability of the gyroscopic system of measurement of the heading, bank and pitch angles of the aerial array. 2 dwg
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Authors
Dates
2003-07-10—Published
2002-03-13—Filed