JPH0625904B2 - Flight simulator - Google Patents
Flight simulatorInfo
- Publication number
- JPH0625904B2 JPH0625904B2 JP15008587A JP15008587A JPH0625904B2 JP H0625904 B2 JPH0625904 B2 JP H0625904B2 JP 15008587 A JP15008587 A JP 15008587A JP 15008587 A JP15008587 A JP 15008587A JP H0625904 B2 JPH0625904 B2 JP H0625904B2
- Authority
- JP
- Japan
- Prior art keywords
- flight
- aircraft
- ground
- control
- program
- 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.)
- Expired - Lifetime
Links
Landscapes
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
Description
【発明の詳細な説明】 ［産業上の利用分野］ 本発明は航空機に搭載される管制システムの地上評価試
験に適用される飛行模擬装置に関する。DETAILED DESCRIPTION OF THE INVENTION [Industrial application] The present invention relates to a flight simulator applied to a ground evaluation test of a control system mounted on an aircraft.
［従来の技術］ 航空機の開発又は管制の改造時、管制システムの評価
は、まず地上において周辺機器を模擬したプログラム評
価装置で行い、その後、自機における飛行試験により実
施される。[Prior Art] When developing an aircraft or modifying a control system, the control system is first evaluated by a program evaluation device that simulates peripheral equipment on the ground, and then a flight test is performed on the aircraft itself.
［発明が解決ようとする問題点］ 地上におけるプログラム評価装置は、周辺機器をコンピ
ュータで模擬している場合が多く、実際の搭載機器との
インターフェイス確認が十分行われない。また自機にて
確認する際、地上においては特異な条件（自機速度がゼ
ロ）でしか実施できないため、すべて飛行試験で確認せ
ざるを得ない。[Problems to be Solved by the Invention] In the program evaluation device on the ground, the peripheral device is often simulated by a computer, and the interface with the actual mounted device is not sufficiently confirmed. In addition, when confirming with your own aircraft, you can only perform it on the ground under unique conditions (own aircraft speed is zero), so you have to confirm everything by flight test.
この発明は地上において自機を使用し、任意の飛行条件
の設定を可能にするものである。The present invention enables the setting of arbitrary flight conditions by using the aircraft itself on the ground.
［問題点を解決するための手段］ この発明の係る飛行模擬装置は、航空機搭載用コンピュ
ータに内蔵された管制プログラム内に、飛行条件を模擬
するプログラムを組み込むことにより地上において任意
の飛行条件を設定可能としたものである。[Means for Solving Problems] A flight simulator according to the present invention sets an arbitrary flight condition on the ground by incorporating a program that simulates a flight condition into a control program built in an aircraft-mounted computer. It was possible.
［作用］ 地上において自機を使用し、任意の飛行条件が設定可能
になることにより、管制システムの基本的な機能が地上
で確認可能になる。[Operation] By using the aircraft itself on the ground and setting arbitrary flight conditions, the basic functions of the control system can be confirmed on the ground.
［実施例］ 第１図は本発明の一実施例をブロック化して示したもの
で、自機に搭載したコンピュータの管制プログラム１０
の一部には、同プログラムの制御の下に、慣性航法装置
からのセンサ信号１に代え、慣性航法装置のコントロー
ルパネルより設定された模擬信号２を処理対象として選
択する切替制御機構１１1，１１2が設けられ、同切替制
御機構１１1，１１2により処理対象ポジションが、ノー
マルポジション側からシミュレートポジション側からシ
ミュレートポジション側に切替わることにより、上記コ
ントロールパネルより設定された模擬信号２に従う飛行
条件による模擬処理が実行される。[Embodiment] FIG. 1 is a block diagram showing an embodiment of the present invention.
Under the control of the program, a switching control mechanism 11 1 for selecting a simulated signal 2 set from a control panel of the inertial navigation device as a processing target instead of the sensor signal 1 from the inertial navigation device. 11 2 is provided, and the switching control mechanisms 11 1 and 11 2 switch the processing target position from the normal position side to the simulated position side to the simulated position side, so that the simulated signal 2 set by the control panel is set. According to the flight conditions, the simulation process is executed.
第１図におけて、飛行諸元の主要センサである慣性航法
装置からの信号１に置き替えると、慣性航法装置のコン
トロールパネルより任意の機体速度及び機体姿勢角の模
擬信号２を設定する。管制プログラム内でコントロール
パネルから入力されたこの模擬信号を使用して、磁気方
位、グランドトラック等の計算を行い、データ設定を行
う。これらの信号号は管制プログラム内で所要の処理を
した後、関連機器へ出力される。したがって機体が地上
に静止している状態時においても模擬信号を設定するこ
とにより任意の飛行状態を作りだすことが可能となる。In FIG. 1, if the signal 1 from the inertial navigation device, which is the main sensor of the flight specifications, is replaced, a simulated signal 2 of an arbitrary aircraft speed and aircraft attitude angle is set from the control panel of the inertial navigation device. Using this simulated signal input from the control panel within the control program, the magnetic direction, ground track, etc. are calculated and data is set. These signal numbers are output to the related equipment after performing necessary processing in the control program. Therefore, even when the airframe is stationary on the ground, it becomes possible to create an arbitrary flight state by setting the simulated signal.
［発明の効果］ 以上述べたように本発明の飛行模擬装置によれば、地上
において自機を使用し、任意の飛行条件が設定可能にな
ることにより、自機地上確認試験で管制システムの基本
機能の確認が容易となり、飛行試験を必要最小限に減ら
すことができる。[Advantages of the Invention] As described above, according to the flight simulator of the present invention, it is possible to set the arbitrary flight conditions by using the aircraft on the ground, and thus the basics of the control system in the aircraft ground confirmation test. The function can be easily confirmed, and flight tests can be reduced to the necessary minimum.
第１図はこの発明の実施例を示す概念図である。 １……センサ信号、２……模擬信号、１０……管制プロ
グラム、１１1，１１2……切替制御機構。FIG. 1 is a conceptual diagram showing an embodiment of the present invention. 1 ... Sensor signal, 2 ... Simulation signal, 10 ... Control program, 11 1 , 11 2 ... Switching control mechanism.
Claims (1)
飛行模擬機能を組み込んだ管制プログラムを有し、同プ
ログラムの制御の下に、上記コンピュータが慣性航法装
置からのセンサ信号に代えて設定された模擬信号を処理
し所定機器へ出力することを特徴とした飛行模擬装置。1. A control program having a flight simulation function of its own built into a computer mounted on an aircraft, wherein the computer is set in place of a sensor signal from an inertial navigation system under the control of the program. A flight simulator which processes the simulated signal and outputs it to a specified device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15008587A JPH0625904B2 (en) | 1987-06-18 | 1987-06-18 | Flight simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP15008587A JPH0625904B2 (en) | 1987-06-18 | 1987-06-18 | Flight simulator |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS63314584A JPS63314584A (en) | 1988-12-22 |
| JPH0625904B2 true JPH0625904B2 (en) | 1994-04-06 |
Family
ID=15489185
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP15008587A Expired - Lifetime JPH0625904B2 (en) | 1987-06-18 | 1987-06-18 | Flight simulator |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0625904B2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2961927B1 (en) * | 2010-06-23 | 2013-12-20 | Turbomeca | REAL TIME SIMULATION SYSTEM FOR THE ENVIRONMENT OF AN AIRCRAFT ENGINE |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS58173789A (en) * | 1982-04-06 | 1983-10-12 | 株式会社日本製鋼所 | Periscope sight training apparatus |
-
1987
- 1987-06-18 JP JP15008587A patent/JPH0625904B2/en not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| JPS63314584A (en) | 1988-12-22 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| S533 | Written request for registration of change of name |
Free format text: JAPANESE INTERMEDIATE CODE: R313533 |
|
| R350 | Written notification of registration of transfer |
Free format text: JAPANESE INTERMEDIATE CODE: R350 |
|
| EXPY | Cancellation because of completion of term |