JPH0313300U - - Google Patents
Info
- Publication number
- JPH0313300U JPH0313300U JP7448389U JP7448389U JPH0313300U JP H0313300 U JPH0313300 U JP H0313300U JP 7448389 U JP7448389 U JP 7448389U JP 7448389 U JP7448389 U JP 7448389U JP H0313300 U JPH0313300 U JP H0313300U
- Authority
- JP
- Japan
- Prior art keywords
- spin
- control
- angular velocity
- stop device
- flying object
- 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
- 238000010586 diagram Methods 0.000 description 3
Landscapes
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Control By Computers (AREA)
Description
第１図はこの考案の一実施例の動作を説明する
ためのフローチヤート図、第２図は従来のスピン
停止装置の結線図、第３図は同じく制御則の線図
、第４図は同じくスピン制御軌跡の線図である。
１……オン・オフ制御器、２……ジエツト・エ
ンジン。
Fig. 1 is a flowchart for explaining the operation of an embodiment of this invention, Fig. 2 is a wiring diagram of a conventional spin stop device, Fig. 3 is a diagram of the control law, and Fig. 4 is the same. It is a diagram of a spin control locus. 1...On/off controller, 2...Jet engine.
Claims (1)
号によりオン・オフ制御器を介して前記飛翔体の
スピンを制御エンジンで停止させるスピン停止装
置において、前記スピン角度および前記スピン角
速度がそれぞれ所定値以下のときは半周方向のス
ピン切替曲線でなる制御則により、その他はスピ
ン極性によりそれぞれ他の制御則によつて前記ス
ピンを制御する制御論理部を備えてなることを特
徴とするスピン停止装置。 In a spin stop device in which the spin of the flying object is stopped by a control engine via an on/off controller based on signals such as a spin angle and a spin angular velocity of the flying object, when the spin angle and the spin angular velocity are each less than a predetermined value. A spin stop device comprising a control logic unit that controls the spin according to a control law based on a spin switching curve in a half-circumferential direction, and other control laws according to spin polarity.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7448389U JPH0313300U (en) | 1989-06-26 | 1989-06-26 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7448389U JPH0313300U (en) | 1989-06-26 | 1989-06-26 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0313300U true JPH0313300U (en) | 1991-02-12 |
Family
ID=31614210
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7448389U Pending JPH0313300U (en) | 1989-06-26 | 1989-06-26 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0313300U (en) |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS517919A (en) * | 1974-03-20 | 1976-01-22 | Piitaa Saimon | |
| JPS5989299A (en) * | 1982-11-09 | 1984-05-23 | 日産自動車株式会社 | Device for changing motion around airframe axis of missile |
-
1989
- 1989-06-26 JP JP7448389U patent/JPH0313300U/ja active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS517919A (en) * | 1974-03-20 | 1976-01-22 | Piitaa Saimon | |
| JPS5989299A (en) * | 1982-11-09 | 1984-05-23 | 日産自動車株式会社 | Device for changing motion around airframe axis of missile |
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