JPH02141600U - - Google Patents
Info
- Publication number
- JPH02141600U JPH02141600U JP11886588U JP11886588U JPH02141600U JP H02141600 U JPH02141600 U JP H02141600U JP 11886588 U JP11886588 U JP 11886588U JP 11886588 U JP11886588 U JP 11886588U JP H02141600 U JPH02141600 U JP H02141600U
- Authority
- JP
- Japan
- Prior art keywords
- aircraft
- attitude
- microcomputer
- actuator
- response
- 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
- 238000001514 detection method Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
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の模式的側面図、第
２図は無重力模擬の代表的飛行パターンを示す線
図、第３図は上記実施例の全体機能の流れを示す
ブロツク図、第４図は別の実施例の全体機能の流
れを示すブロツク図である。
１…航空機、２…実験装置本体、３…実験装置
取付台、４…ヒンジ、５…油圧アクチユエータ、
６…制御装置、７…マイクロコンピユータ、８…
航空機姿勢検知センサ。
Fig. 1 is a schematic side view of one embodiment of the present invention, Fig. 2 is a line diagram showing a typical flight pattern for simulating zero gravity, Fig. 3 is a block diagram showing the overall functional flow of the above embodiment, and Fig. FIG. 4 is a block diagram showing the overall functional flow of another embodiment. DESCRIPTION OF SYMBOLS 1...Aircraft, 2...Experiment equipment main body, 3...Experiment equipment mounting stand, 4...Hinge, 5...Hydraulic actuator,
6...control device, 7...microcomputer, 8...
Aircraft attitude detection sensor.
Claims (1)
ンピユータと、同マイクロコンピユータの出力に
応じて作動するアクチユエータと、同アクチユエ
ータの作動により航空機の姿勢変化による傾きを
補正して一定姿勢を保つ実験装置本体とを具備し
てなることを特徴とする航空機の無重力実験装置
。 A microcomputer that outputs output in response to changes in the attitude of the aircraft, an actuator that operates in response to the output of the microcomputer, and an experimental device that maintains a constant attitude by correcting the tilt caused by changes in the attitude of the aircraft through the operation of the actuator. A zero-gravity experimental device for an aircraft, characterized by comprising:
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11886588U JPH02141600U (en) | 1988-09-12 | 1988-09-12 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP11886588U JPH02141600U (en) | 1988-09-12 | 1988-09-12 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH02141600U true JPH02141600U (en) | 1990-11-28 |
Family
ID=31667008
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP11886588U Pending JPH02141600U (en) | 1988-09-12 | 1988-09-12 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH02141600U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2558258A1 (en) * | 2014-07-31 | 2016-02-02 | Universitat Politècnica De Catalunya | Simulation device of absence of gravity in an aircraft (Machine-translation by Google Translate, not legally binding) |
-
1988
- 1988-09-12 JP JP11886588U patent/JPH02141600U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2558258A1 (en) * | 2014-07-31 | 2016-02-02 | Universitat Politècnica De Catalunya | Simulation device of absence of gravity in an aircraft (Machine-translation by Google Translate, not legally binding) |
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