发明名称 GUIDED MISSILE FIRING METHOD
摘要 FIELD: weapons and ammunition.SUBSTANCE: performed is topographic control of target indicator and launching facility to the terrain by ground satellite receiver, determined are coordinates of launching facility and location and ephemeris for each space vehicle of satellite positioning system, detected and measured are target coordinates, the coordinates are transmitted to artillery position control station, set is universal computer time in reconnaissanceman's console and artillery position control station, calculated and transmitted are shooting settings to launching facility automatic control unit, performed is missile launching procedure, the missile is launched from transporter-launcher container along the preset ballistic course, the missile is oriented by on-board navigation satellite receiver, when the missile approaches the target it is oriented by laser emitter.EFFECT: providing higher probability of guided missile hitting the target.
申请公布号 RU2538509(C1) 申请公布日期 2015.01.10
申请号 RU20130130684 申请日期 2013.07.03
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "KONSTRUKTORSKOE BJURO PRIBOROSTROENIJA IM. AKADEMIKA A.G. SHIPUNOVA" 发明人 GUSEV ANDREJ VIKTOROVICH;OBRAZUMOV VLADIMIR IVANOVICH;PODCHUFAROV JURIJ BORISOVICH;OVSENEV SERGEJ SERGEEVICH;SEL'KIN VLADISLAV VLADIMIROVICH;LARIN DMITRIJ VIKTOROVICH;KUSHNIKOV DMITRIJ VJACHESLAVOVICH;ZEMTSOV ROMAN NIKOLAEVICH;LARIN ANDREJ VIKTOROVICH
分类号 F42B15/01 主分类号 F42B15/01
代理机构 代理人
主权项
地址