JPS62125895U - - Google Patents
Info
- Publication number
- JPS62125895U JPS62125895U JP1986009735U JP973586U JPS62125895U JP S62125895 U JPS62125895 U JP S62125895U JP 1986009735 U JP1986009735 U JP 1986009735U JP 973586 U JP973586 U JP 973586U JP S62125895 U JPS62125895 U JP S62125895U
- Authority
- JP
- Japan
- Prior art keywords
- control device
- guidance
- moving object
- flying object
- target
- 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
- 230000001133 acceleration Effects 0.000 claims description 2
- 230000000087 stabilizing effect Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 2
Description
第１図は、この考案を適用した飛しよう体の誘
導制御系のブロツク図、第２図は、従来の誘導制
御系のブロツク図、図中、１は受信信号処理部、
２は駆動回路部、３はレートジヤイロ、４は誘導
計算部、５は補償部、６は翼駆動部、７は機体特
性〔１〕，８は機体特性〔２〕，９は加速度計、
１０は飛しよう体用レートジヤイロ、１１は加速
度信号ゲイン調整器である。なお、図中同一ある
いは相当部分には同一符号を付してある。
Fig. 1 is a block diagram of a guidance and control system for a flying object to which this invention is applied, and Fig. 2 is a block diagram of a conventional guidance and control system.
2 is a drive circuit section, 3 is a rate gyro, 4 is a guidance calculation section, 5 is a compensation section, 6 is a wing drive section, 7 is an airframe characteristic [1], 8 is an airframe characteristic [2], 9 is an accelerometer,
10 is a rate gyro for flying bodies, and 11 is an acceleration signal gain adjuster. In addition, the same reference numerals are given to the same or corresponding parts in the figures.
Claims (1)
標の相対位置を検出し追尾する誘導装置と、上記
誘導装置からの信号により飛しよう体を目標の方
向に制御する制御装置と、上記制御装置内で得ら
れる飛しよう体の加速度信号を処理する回路とを
備えたことを特徴とする運動体の誘導装置。 A guidance device that has a function of stabilizing in inertial space and detects and tracks the relative position of a moving object and a target, a control device that controls the flying object in the direction of the target based on a signal from the guidance device, and the control device described above. 1. A device for guiding a moving object, comprising: a circuit for processing an acceleration signal of the flying object obtained within the device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1986009735U JPS62125895U (en) | 1986-01-27 | 1986-01-27 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1986009735U JPS62125895U (en) | 1986-01-27 | 1986-01-27 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS62125895U true JPS62125895U (en) | 1987-08-10 |
Family
ID=30795328
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1986009735U Pending JPS62125895U (en) | 1986-01-27 | 1986-01-27 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62125895U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH04110600A (en) * | 1990-01-01 | 1992-04-13 | Hughes Aircraft Co | Lightweight missile guidance system |
-
1986
- 1986-01-27 JP JP1986009735U patent/JPS62125895U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH04110600A (en) * | 1990-01-01 | 1992-04-13 | Hughes Aircraft Co | Lightweight missile guidance system |
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