发明名称 METHOD FOR GUIDANCE OF GUIDED MISSILE
摘要 FIELD: military equipment, in particular, methods for guidance of guided missiles installed as a part of complexes of guided missile armament both on ground launchers and on various objectives, such as tanks, infantry fighting vehicles, self-propelled launchers, etc. ^ SUBSTANCE: in the process of formation of the sight line, alignment of it with the target, measurement by the guidance system of the deviation of the guided missile from the sight line, automatic formation of the control command and transmission of it to the missile, generation of a signal corresponding to this command and delivery of it to the missile control members, formation of the second sight line and alignment of it with the target, measurement of missile deviation from it, formation of the second control command and generation of a signal to the missile control members in compliance with the sum of the first and second control commands, additionally measured are the angular velocities of the sight lines, determined is the larger of them by the modulus and summed up with the signal supplied by the missile to the control members. ^ EFFECT: enhanced efficiency of guidance of the guided missile. ^ 1 dwg
申请公布号 RU2240486(C1) 申请公布日期 2004.11.20
申请号 RU20030133123 申请日期 2003.11.13
申请人 发明人 DEM'JANENKO A.V.;STAROSTIN M.M.;TKACHENKO V.I.
分类号 F41G3/22 主分类号 F41G3/22
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