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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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