发明名称 Sökare för målförföljande missiler
摘要 The seeker for a guided missile has a Cardan frame (18,22) carrying an electro-optical seeker (16) assembly which aligns on a target beam. Actuators (36,38) align the seeker assembly onto the target. The seeker assembly has a single roll axis (42) and a perpendicular pitch axis (20) to support it in the missile airframe. The rotational angle of the seeker is read by a monitor (28) and an inertial sensor (48) measures the angular velocity around the three perpendicular axes.
申请公布号 SE9403070(L) 申请公布日期 2003.01.05
申请号 SE19940003070 申请日期 1994.09.14
申请人 BODENSEEWERK GERAETETECH 发明人 HARTMANN U;SCHNATZ J;GOSEBERG H
分类号 F41G7/22;F42B30/00;G01S3/786;(IPC1-7):F41G7/22 主分类号 F41G7/22
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