JPS6443411U - - Google Patents
Info
- Publication number
- JPS6443411U JPS6443411U JP13648987U JP13648987U JPS6443411U JP S6443411 U JPS6443411 U JP S6443411U JP 13648987 U JP13648987 U JP 13648987U JP 13648987 U JP13648987 U JP 13648987U JP S6443411 U JPS6443411 U JP S6443411U
- Authority
- JP
- Japan
- Prior art keywords
- flapper
- right nozzles
- roll
- control device
- switches
- 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 2
- 239000000567 combustion gas Substances 0.000 claims 1
- 238000002347 injection Methods 0.000 claims 1
- 239000007924 injection Substances 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 3
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Description
第１図は本考案の一実施例を示す構成図、第２
図は従来のロール制御装置を示す構成図、第３図
は同従来のロール制御装置を備えたロケツトの尾
翼まわりを示す平面図、第４図は同従来の作用説
明図である。
１……ロケツト（飛翔体）、３……モータチヤ
ンバ、４……左ノズル、５……右ノズル、６……
フラツパ、８……姿勢検出基準部、１９……フラ
ツパアクチユエータ、２１……電流制御部、Ｅｓ
……ロール誤差信号、Ｉ……駆動電流。
Fig. 1 is a configuration diagram showing one embodiment of the present invention;
FIG. 3 is a block diagram showing a conventional roll control device, FIG. 3 is a plan view showing the area around the tail wing of a rocket equipped with the conventional roll control device, and FIG. 4 is an explanatory diagram of the operation of the conventional roll control device. 1...Rocket (flying object), 3...Motor chamber, 4...Left nozzle, 5...Right nozzle, 6...
Flutter, 8... Attitude detection reference unit, 19... Flapper actuator, 21... Current control unit, Es
...Roll error signal, I...Drive current.
Claims (1)
ノズルと、モータチヤンバから左右ノズルに導出
される燃焼ガスの噴射方向を切り替えるフラツパ
と、姿勢検出基準部側からのロール誤差信号の大
きさに応じてフラツパアクチユエータの駆動電流
を制御する電流制御部とを備えたことを特徴とす
る飛翔体のロール制御装置。 The left and right nozzles are arranged toward the circumferential direction of the aircraft's body axis, the flapper switches the injection direction of the combustion gas guided from the motor chamber to the left and right nozzles, and the flapper switches depending on the magnitude of the roll error signal from the attitude detection reference section. 1. A roll control device for a flying object, comprising: a current control unit that controls a drive current of a flapper actuator;
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13648987U JPS6443411U (en) | 1987-09-07 | 1987-09-07 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP13648987U JPS6443411U (en) | 1987-09-07 | 1987-09-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6443411U true JPS6443411U (en) | 1989-03-15 |
Family
ID=31397049
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP13648987U Pending JPS6443411U (en) | 1987-09-07 | 1987-09-07 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6443411U (en) |
-
1987
- 1987-09-07 JP JP13648987U patent/JPS6443411U/ja active Pending
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