JPS62185698U - - Google Patents
Info
- Publication number
- JPS62185698U JPS62185698U JP7465586U JP7465586U JPS62185698U JP S62185698 U JPS62185698 U JP S62185698U JP 7465586 U JP7465586 U JP 7465586U JP 7465586 U JP7465586 U JP 7465586U JP S62185698 U JPS62185698 U JP S62185698U
- Authority
- JP
- Japan
- Prior art keywords
- horizontal
- accelerometer
- vertical
- acceleration
- rudder angle
- 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 6
- 238000010586 diagram Methods 0.000 description 2
Landscapes
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
Description
第１図は本考案の一実施例を示す構成説明図、
第２図は航空機の０Ｇ飛行の一例を示す説明図で
ある。
１１……垂直方向加速度計、１２……水平方向
加速度計、１３……自動制御用コンピユータ、１
４……スロツトル・コントロールオーパイアクチ
ユエータ、１５……エレベータ・コントロールオ
ーパイサーボ、１６……エンジン、１７……エレ
ベータアクチユエータ、１８……エレベータ舵面
、１９……スピードブレーキアクチユエータ、２
０……スピードブレーキ舵面。
FIG. 1 is a configuration explanatory diagram showing an embodiment of the present invention;
FIG. 2 is an explanatory diagram showing an example of 0G flight of an aircraft. 11...Vertical accelerometer, 12...Horizontal accelerometer, 13...Automatic control computer, 1
4...Throttle control overpass actuator, 15...Elevator control overpass servo, 16...Engine, 17...Elevator actuator, 18...Elevator control surface, 19...Speed brake actuator, 2
0...Speed brake control surface.
Claims (1)
び水平方向加速度を検出する水平方向加速度計と
、この水平方向加速度計で検出された水平方向加
速度及び前記垂直方向加速度計で検出された垂直
方向加速度が入力され航空機の０Ｇを保持させる
舵角制御信号を計算する自動制御用コンピユータ
と、このコンピユータからの舵角制御信号でアク
チユエータにより舵角を駆動させ水平方向加速度
および垂直方向加速度をそれぞれ０に保持する装
置とを具備することを特徴とする航空機の０Ｇ保
持制御装置。 A vertical accelerometer that detects vertical acceleration and a horizontal accelerometer that detects horizontal acceleration, and the horizontal acceleration detected by this horizontal accelerometer and the vertical acceleration detected by the vertical accelerometer are input. an automatic control computer that calculates a rudder angle control signal that maintains the aircraft at 0G; and a device that uses the rudder angle control signal from this computer to drive the rudder angle by an actuator to maintain horizontal acceleration and vertical acceleration at 0. A 0G holding control device for an aircraft, comprising:
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7465586U JPS62185698U (en) | 1986-05-20 | 1986-05-20 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7465586U JPS62185698U (en) | 1986-05-20 | 1986-05-20 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS62185698U true JPS62185698U (en) | 1987-11-26 |
Family
ID=30920068
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7465586U Pending JPS62185698U (en) | 1986-05-20 | 1986-05-20 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62185698U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0310999A (en) * | 1989-06-07 | 1991-01-18 | Natl Space Dev Agency Japan<Nasda> | Micro-gravity experiment device using aircraft |
| WO2014200084A1 (en) * | 2013-06-13 | 2014-12-18 | 株式会社スペース・バイオ・ラボラトリーズ | Gravity control device |
-
1986
- 1986-05-20 JP JP7465586U patent/JPS62185698U/ja active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0310999A (en) * | 1989-06-07 | 1991-01-18 | Natl Space Dev Agency Japan<Nasda> | Micro-gravity experiment device using aircraft |
| WO2014200084A1 (en) * | 2013-06-13 | 2014-12-18 | 株式会社スペース・バイオ・ラボラトリーズ | Gravity control device |
| JP2015000008A (en) * | 2013-06-13 | 2015-01-05 | 株式会社スペース・バイオ・ラボラトリーズ | Gravity control device |
| EP3009499A4 (en) * | 2013-06-13 | 2016-12-07 | Space Bio-Laboratories Co Ltd | Gravity control device |