JPS6361698U - - Google Patents
Info
- Publication number
- JPS6361698U JPS6361698U JP15415686U JP15415686U JPS6361698U JP S6361698 U JPS6361698 U JP S6361698U JP 15415686 U JP15415686 U JP 15415686U JP 15415686 U JP15415686 U JP 15415686U JP S6361698 U JPS6361698 U JP S6361698U
- Authority
- JP
- Japan
- Prior art keywords
- roll angle
- target
- gimbal
- detects
- missile
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000001514 detection method Methods 0.000 claims description 3
- 230000000007 visual effect Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 2
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Description
第１図はこの考案に係るミサイルシーカの一実
施例を示す構成図、第２図は及び第３図はそれぞ
れ同実施例の動作を示す図、第４図は従来のミサ
イルシーカの構成を示す構成図である。
１……ミサイルきよう体、２……目標検知器、
３……シーカジンバル、４……ジンバル取付面、
５……機体軸、６……視野範囲、７……目標位置
検出部、８……ロール制御部、９……ロール角検
出部、１０，１１……ロール舵。
Fig. 1 is a configuration diagram showing an embodiment of the missile seeker according to this invention, Figs. 2 and 3 are diagrams showing the operation of the same embodiment, and Fig. 4 shows the configuration of a conventional missile seeker. FIG. 1...Missile target body, 2...Target detector,
3...Seeka gimbal, 4...Gimbal mounting surface,
5... Body axis, 6... View range, 7... Target position detection section, 8... Roll control section, 9... Roll angle detection section, 10, 11... Roll rudder.
Claims (1)
り付けられるシーカジンバルと、このシーガンバ
ルで得られる目標信号から目標方位角を検出する
目標位置検出部と、ミサイル機体のロール角を検
出するロール角検出部と、前記目標方位角及びロ
ール角に基づいて前記シーカジンバルの視野範囲
中心が目標方位方向となるようにミサイル機体の
ロール角を制御するロール角制御手段とを具備す
るミサイルシーカ。 A seeker gimbal installed at a constant inclination with respect to the missile body axis, a target position detection unit that detects the target azimuth from the target signal obtained by this sea gun gimbal, and a roll angle detector that detects the roll angle of the missile body. and roll angle control means for controlling the roll angle of the missile aircraft so that the center of the visual field of the seeker gimbal is in the target azimuth direction based on the target azimuth angle and roll angle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15415686U JPS6361698U (en) | 1986-10-07 | 1986-10-07 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15415686U JPS6361698U (en) | 1986-10-07 | 1986-10-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6361698U true JPS6361698U (en) | 1988-04-23 |
Family
ID=31073694
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP15415686U Pending JPS6361698U (en) | 1986-10-07 | 1986-10-07 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6361698U (en) |
-
1986
- 1986-10-07 JP JP15415686U patent/JPS6361698U/ja active Pending
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