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
Application number
JP11886588U
Other languages
Japanese (ja)
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed filed Critical
Priority to JP11886588U priority Critical patent/JPH02141600U/ja
Publication of JPH02141600U publication Critical patent/JPH02141600U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Description

【図面の簡単な説明】[Brief explanation of drawings]

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)

【実用新案登録請求の範囲】[Scope of utility model registration request] 航空機の姿勢変化に応じて出力するマイクロコ
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:
JP11886588U 1988-09-12 1988-09-12 Pending JPH02141600U (en)

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)

* Cited by examiner, † Cited by third party
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)

Cited By (1)

* Cited by examiner, † Cited by third party
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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