发明名称 GUIDED MISSILE GUIDANCE SYSTEM
摘要 FIELD: weapons. ^ SUBSTANCE: invention relates to guidance systems and can be incorporated with tank and antitank complexes as well as in small-size antiaircraft complexes. Control station additionally incorporates unit to generate two flat orthogonal beams, course- and pitch-scanned perpendicular to their planes, which adds to security of control process due to small instantaneous area and short duration of terrain illumination in target area. Control station also incorporates synchroniser and unit to generate codes and pulse codes transmitting, on scanned beams, the data on spatial position in the form of time-pulse modulation in preset, for given complex, level of security to increase efficiency in simultaneous fire from several complexes and provide security of control thanks to pulsed radiation mode (minor radiation power). Missile incorporates unit to gate received signal, gate pulse unit, onboard pulse code synchroniser and analyser to extract missile coordinates transmitted on their pulse code level. ^ EFFECT: higher noise immunity and accuracy thanks to generation and transmission of commands of dynamic error compensation. ^ 3 dwg
申请公布号 RU2382315(C1) 申请公布日期 2010.02.20
申请号 RU20080128977 申请日期 2008.07.15
申请人 GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "KONSTRUKTORSKOE BJURO PRIBOROSTROENIJA" 发明人 MOROZOV VLADIMIR IVANOVICH;NEDOSEKIN IGOR' ALEKSEEVICH;MINAKOV VLADIMIR MIKHAJLOVICH;NAZAROV JURIJ MIKHAJLOVICH;TARASOV VIKTOR IVANOVICH
分类号 F41G7/26 主分类号 F41G7/26
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