发明名称 SMALL-SIZE AIRCRAFT TARGET HOMING SYSTEM
摘要 FIELD: radio engineering, communication.SUBSTANCE: system comprises an antenna, an autodyne radar with two outputs, an electronic switch, a memory unit, a first computing unit, a second computing unit, a logic device, a control device a timer and a deviation signal estimation unit, comprising n threshold devices, signal setting devices and an OR element. The output of the second computing unit is connected to the input of the deviation signal estimation unit, the inputs of which are the first inputs of the n threshold devices, the second inputs of which are connected to the outputs of the signal setting devices, and the outputs of the n threshold devices are connected to inputs of the OR element, the output of which is the output of the deviation signal estimation unit.EFFECT: high accuracy of guiding guided missiles to a target by taking into account the deviation of the missile from the missile-target line of sight.3 dwg
申请公布号 RU2539824(C1) 申请公布日期 2015.01.27
申请号 RU20130149430 申请日期 2013.11.06
申请人 EFANOV VASILIJ VASIL'EVICH;VASETSKIJ VIKTOR VITAL'EVICH;KOSAREV GRIGORIJ GENNAD'EVICH;PLIPLIN ANDREJ ALEKSANDROVICH 发明人 EFANOV VASILIJ VASIL'EVICH;VASETSKIJ VIKTOR VITAL'EVICH;KOSAREV GRIGORIJ GENNAD'EVICH;PLIPLIN ANDREJ ALEKSANDROVICH
分类号 F41G7/00 主分类号 F41G7/00
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