JPS59148999U - Guided flying vehicle control device - Google Patents
Guided flying vehicle control deviceInfo
- Publication number
- JPS59148999U JPS59148999U JP543784U JP543784U JPS59148999U JP S59148999 U JPS59148999 U JP S59148999U JP 543784 U JP543784 U JP 543784U JP 543784 U JP543784 U JP 543784U JP S59148999 U JPS59148999 U JP S59148999U
- Authority
- JP
- Japan
- Prior art keywords
- guided flying
- flying object
- control device
- control
- vehicle control
- 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
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第１図は従来の誘導飛翔体の操舵制御装置により飛翔体
が目標をホーミングする状態を説明するために示す図、
第２図は本考案の一実施例を示す′図、第３図は振り子
のなす傾きを検出す名手段を示す構成説明図、゛第４図
ａ、 ｂは正弦波ポテンションメータ部を示す図、第
４図ｃ、 ｄはそれぞれ正弦波ポテンションメータ部の
出力を示す波形図である。 −
２１・・・飛翔体、２２． ２３． ２４． ２５・・
・操縦翼、２７・・・振り子。FIG. 1 is a diagram shown to explain a state in which a flying object is homing to a target using a conventional steering control device for a guided flying object.
Fig. 2 shows an embodiment of the present invention, Fig. 3 is a configuration explanatory diagram showing a famous means for detecting the inclination of a pendulum, and Fig. 4 a and b show a sine wave potentiometer section. 4c and 4d are waveform diagrams showing the output of the sine wave potentiometer section, respectively. - 21... Flying object, 22. 23. 24. 25...
- Control wing, 27...pendulum.
Claims (1)
飛翔体と、この誘導飛翔体の内部に設けられ機軸周りの
みに回転自由に重心偏心のある振り子と、この振り子の
垂下方向に応じて前記操縦翼の配列方向と目標方向との
差を検出する手段と、この手段による差信号によって前
記操縦翼を制御し目標が前記操縦翼の仰角内に位置する
如く前記飛翔体をパンクせしめる制御手段とを具備した
ことを特徴とする誘導飛翔体の操舵制御装置。A guided flying object having control wings arranged in a cross with the aircraft axis as the center; a pendulum provided inside the guided flying object with an eccentric center of gravity that can freely rotate only around the aircraft axis; means for detecting a difference between the arrangement direction of the control blades and the target direction; and control means for controlling the control blades based on the difference signal from the means to puncture the flying object so that the target is located within the elevation angle of the control blades. A steering control device for a guided flying object, characterized by comprising:
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP543784U JPS59148999U (en) | 1984-01-19 | 1984-01-19 | Guided flying vehicle control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP543784U JPS59148999U (en) | 1984-01-19 | 1984-01-19 | Guided flying vehicle control device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS59148999U true JPS59148999U (en) | 1984-10-04 |
Family
ID=30137025
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP543784U Pending JPS59148999U (en) | 1984-01-19 | 1984-01-19 | Guided flying vehicle control device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59148999U (en) |
-
1984
- 1984-01-19 JP JP543784U patent/JPS59148999U/en active Pending
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