发明名称 GUIDED MISSILE GUIDANCE SYSTEM
摘要 FIELD: optical guidance systems, applicable in guided missile teleorientation systems in laser beams. SUBSTANCE: optical sight of the guidance system, having a sight channel and a guidance channel including a source of laser radiation, modulator and a forming optical system with a variable focal length, uses an optical system control circuit, and the guided missile uses a driver of missile criterion according to the type of ballistic characteristics, whose output before missile launching is connected to the first input of the control circuit, whose second input is connected to the missile launching system, and the output - to the optical system with a variable focal length. EFFECT: unified guidance system for missiles with different ballistic characteristics. 3 cl, 2 dwg
申请公布号 RU2126522(C1) 申请公布日期 1999.02.20
申请号 RU19970120321 申请日期 1997.11.25
申请人 KONSTRUKTORSKOE BJURO PRIBOROSTROENIJA 发明人 DOLGOV V.V.;MATVEEV EH.L.;PANFILOV JU.A.;POGOREL'SKIJ S.L.;TELYSHEV V.A.;SHIPUNOV A.G.
分类号 F41G7/26;F42B15/00;(IPC1-7):F41G7/26 主分类号 F41G7/26
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