WEKO3
アイテム
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定点滞空飛行試験成果報告書:試験システム及び飛行試験結果
https://jaxa.repo.nii.ac.jp/records/2225
https://jaxa.repo.nii.ac.jp/records/22252f7ae837-853c-4881-bb8f-716786a0cd2c
名前 / ファイル | ライセンス | アクション |
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63454000.pdf (25.8 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||||
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公開日 | 2015-03-26 | |||||||
タイトル | ||||||||
タイトル | 定点滞空飛行試験成果報告書:試験システム及び飛行試験結果 | |||||||
言語 | ||||||||
言語 | jpn | |||||||
キーワード | ||||||||
主題Scheme | Other | |||||||
主題 | 成層圏プラットフォーム飛行船 | |||||||
キーワード | ||||||||
主題Scheme | Other | |||||||
主題 | 成層圏 | |||||||
キーワード | ||||||||
主題Scheme | Other | |||||||
主題 | 定点飛行試験 | |||||||
キーワード | ||||||||
主題Scheme | Other | |||||||
主題 | 気球飛翔 | |||||||
キーワード | ||||||||
主題Scheme | Other | |||||||
主題 | 気球観測 | |||||||
キーワード | ||||||||
主題Scheme | Other | |||||||
主題 | 高高度気球 | |||||||
キーワード | ||||||||
主題Scheme | Other | |||||||
主題 | 空気力 | |||||||
キーワード | ||||||||
主題Scheme | Other | |||||||
主題 | 空力特性 | |||||||
キーワード | ||||||||
主題Scheme | Other | |||||||
主題 | 空力抵抗 | |||||||
キーワード | ||||||||
主題Scheme | Other | |||||||
主題 | 自律航法 | |||||||
キーワード | ||||||||
言語 | en | |||||||
主題Scheme | Other | |||||||
主題 | stratospheric platform airship | |||||||
キーワード | ||||||||
言語 | en | |||||||
主題Scheme | Other | |||||||
主題 | stratosphere | |||||||
キーワード | ||||||||
言語 | en | |||||||
主題Scheme | Other | |||||||
主題 | stationary flight test | |||||||
キーワード | ||||||||
言語 | en | |||||||
主題Scheme | Other | |||||||
主題 | balloon flight | |||||||
キーワード | ||||||||
言語 | en | |||||||
主題Scheme | Other | |||||||
主題 | balloon sounding | |||||||
キーワード | ||||||||
言語 | en | |||||||
主題Scheme | Other | |||||||
主題 | high altitude balloon | |||||||
キーワード | ||||||||
言語 | en | |||||||
主題Scheme | Other | |||||||
主題 | aerodynamic force | |||||||
キーワード | ||||||||
言語 | en | |||||||
主題Scheme | Other | |||||||
主題 | aerodynamic characteristic | |||||||
キーワード | ||||||||
言語 | en | |||||||
主題Scheme | Other | |||||||
主題 | aerodynamic drag | |||||||
キーワード | ||||||||
言語 | en | |||||||
主題Scheme | Other | |||||||
主題 | autonomous navigation | |||||||
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(英) | ||||||||
その他のタイトル | Low altitude stationary flight test: Test vehicle and flight test results | |||||||
著者 |
宇宙航空研究開発機構定点滞空飛行試験実験隊
× 宇宙航空研究開発機構定点滞空飛行試験実験隊× Low Altitude Stationary Flight Test Team, Japan Aerospace Exploration Agency
WEKO
4437
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著者所属 | ||||||||
宇宙航空研究開発機構 | ||||||||
著者所属(英) | ||||||||
en | ||||||||
Japan Aerospace Exploration Agency | ||||||||
出版者 | ||||||||
出版者 | 宇宙航空研究開発機構 | |||||||
出版者(英) | ||||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||||
書誌情報 |
宇宙航空研究開発機構研究開発報告 en : JAXA Research and Development Report 巻 JAXA-RR-06-010, 発行日 2007-03-30 |
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抄録 | ||||||||
内容記述タイプ | Abstract | |||||||
内容記述 | 成層圏プラットフォーム飛行船の鍵となる技術を実証すると共に、各種ミッション試験を実施すべく、定点滞空試験機の飛行試験を実施した。定点滞空試験機は、全長68mの無人飛行船であり、遠隔操縦または自律で飛行する。試験機は合計8フライト飛行、最後の3フライトでは、自律による定点滞空飛行を実施、約900mと2kmの高度に於いて地球観測ミッションに成功、4kmおよび4km近傍の高度に於いて通信放送ミッションに成功した。本稿では、定点滞空試験機の開発および定点滞空飛行試験について:(1)プロジェクトの概要;(2)系統ごとの試験システムの構成および関連する開発試験、追跡管制系との噛み合わせ試験;(3)飛行試験計画から実施に至る、飛行試験実施作業;(4)第1段階から第3段階の各飛行の概要および系統毎の結果を含む飛行試験結果、について報告する。ハイテク膜材製の試験機船体構造は、試験期間中健全であり、安全な運用に供し得ることが確認された。熱浮力制御は、実飛行状態で海面から4kmの高度まで有効であった。定点滞空精度は設計要求内であり、飛行誘導制御則が妥当であることが確認された。以上、目的は総て達成され、定点滞空飛行試験は成功裡に終了した。 | |||||||
抄録(英) | ||||||||
内容記述タイプ | Other | |||||||
内容記述 | A series of flight tests was conducted with the SPF-2 low-altitude stationary flight test vehicle to demonstrate and prove key technologies for Stratospheric PlatForm (SPF) airships while conducting experiments for various missions. The SPF-2 is a 68.4 m long unmanned non-rigid airship that can fly autonomously or be controlled from its ground station through a communication link. Starting with vertical takeoff/landing flights (tethered and non-tethered) over the ground handling area, the flight test vehicle made a total of eight flights. In the last three tests, autonomous geostationary flights were made, including the successful gathering of earth environment and traffic observations at altitudes of approximately 900 m and 2 km, and telecommunications and broadcasting missions at and near 4 km. This report on SPF-2 flight tests begins with an overview of the project, followed by descriptions of: (1) the systems that constitute the vehicle; (2) various tests conducted in the course of SPF-2 development including system integration with the tracking and command system; (3) tasks undertaken from planning to testing stages; (4) flight test results in each technical field. The structure of the hull envelope, made of high-technology thin membrane materials, remained sound throughout the testing program, confirming its operational reliability and safety. Buoyancy control and thermal management were effective in real flight from sea level to 4 km altitude, and it was confirmed that the control and guidance laws were adequate. In summary, the development of the SPF-2 was successful, with the objectives fully achieved. | |||||||
ISSN | ||||||||
収録物識別子タイプ | ISSN | |||||||
収録物識別子 | 1349-1113 | |||||||
書誌レコードID | ||||||||
収録物識別子タイプ | NCID | |||||||
収録物識別子 | AA1192675X | |||||||
資料番号 | ||||||||
内容記述タイプ | Other | |||||||
内容記述 | 資料番号: AA0063454000 | |||||||
レポート番号 | ||||||||
内容記述タイプ | Other | |||||||
内容記述 | レポート番号: JAXA-RR-06-010 |