发明名称 |
Radar seeker transient suppressor |
摘要 |
PCT No. PCT/GB89/00088 Sec. 371 Date Sep. 11, 1989 Sec. 102(e) Date Sep. 11, 1989 PCT Filed Jan. 30, 1989 PCT Pub. No. WO89/07231 PCT Pub. Date Aug. 10, 1989.A radar seeker transient suppressor for an anti-radar homing missile in which glint effects upset the smooth tracking of a target by apparently changing the target position spasmodically. A seeker output signal is derived which is at least substantially independent of body movement e.g. the target sightline angle signal rather than the look angle signal (i.e. relative to a space reference rather than a body reference). This signal is used to control the steering either filtered or unfiltered according to whether the difference exceeds a threshold value or not. Both azimuth and elevation channels are treated similarly and in unison. An excessive filtered/unfiltered difference in either channel causes use of the filtered signal in both. A double integrating filter may be employed to avoid the relative displacement of output and input signals when the input is, or contains, a ramp component.
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申请公布号 |
US4991794(A) |
申请公布日期 |
1991.02.12 |
申请号 |
US19890399490 |
申请日期 |
1989.09.11 |
申请人 |
THE MARCONI COMPANY LIMITED |
发明人 |
BENSON, ANTHONY J.;PEW, FREDERICK L.;WALTER, OLIVER H. D.;WARMAN, GEOFFREY;JONES, MICHAEL A. |
分类号 |
F41G7/22;G05D1/12 |
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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