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Development of the Triplex Digital Flight Control System of the STOL Research Aircraft “ASKA”
https://jaxa.repo.nii.ac.jp/records/45272
https://jaxa.repo.nii.ac.jp/records/45272bd566632-22db-4606-911f-a4dd755fe644
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
naltr01013.pdf (14.3 MB)
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| Item type | テクニカルレポート / Technical Report(1) | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| 公開日 | 2015-03-26 | |||||||||
| タイトル | ||||||||||
| タイトル | Development of the Triplex Digital Flight Control System of the STOL Research Aircraft “ASKA” | |||||||||
| 言語 | en | |||||||||
| 言語 | ||||||||||
| 言語 | eng | |||||||||
| 資源タイプ | ||||||||||
| 資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||||||
| 資源タイプ | technical report | |||||||||
| その他のタイトル | ||||||||||
| その他のタイトル | STOL実験機SCAS開発概要 | |||||||||
| 著者 |
STOLプロジェクト推進本部機体技術開発室飛行試験室
× STOLプロジェクト推進本部機体技術開発室飛行試験室
× Flight Control System Development Team STOL Research Aircraft Project Group
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| 著者所属 | ||||||||||
| 航空宇宙技術研究所 | ||||||||||
| 著者所属（英） | ||||||||||
| en | ||||||||||
| National Aerospace Laboratory(NAL) | ||||||||||
| 出版者 | ||||||||||
| 出版者 | 航空宇宙技術研究所 | |||||||||
| 出版者（英） | ||||||||||
| 出版者 | National Aerospace Laboratory(NAL) | |||||||||
| 書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-1013 巻 1013, p. 91, 発行日 1989-02 |
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| 抄録（英） | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | National Aerospace Laboratory has been developing the STOL research aircraft named “ASKA” which underwent its maiden flight on October 28th, 1985. This project was started for the purpose of establishing STOL technology in Japan. In order to improve the stability and control of the ASKA in the low air speed region, the ASKA has a triplex digital stability and control augmentation system (SCAS) in which new technologies are introduced. This paper describes the outline of design objectives, functions, a series of development tests and results of the SCAS which include triplex digital computer systems, a triplex force summing electro hydraulic series servo actuator, a head-up display and a low airspeed sensor. Most of the development tests were devoted to verifying the system hardware and software through control system functional mockup tests, and flight simulator tests connecting with the digital computer systems. And finally the overall functions of the SCAS were tested in actual flight. The problems encountered during these tests are also presented. | |||||||||
| ISSN | ||||||||||
| 収録物識別子タイプ | ISSN | |||||||||
| 収録物識別子 | 0389-4010 | |||||||||
| 資料番号 | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | 資料番号: NALTR1013000 | |||||||||
| レポート番号 | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | レポート番号: NAL TR-1013 | |||||||||
