著者・編者STOLプロジェクト推進本部実験機開発操縦システム技術開発チーム
STOL Aircraft Project Group
並列タイトル等STOL実験機「飛鳥」の操縦系統機能試験計画と機械系操縦系統試験結果について
タイトル(掲載誌)航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-944
一般注記出版タイプ: NA
The control system of the National Aerospace Laboratory Quiet-STOL Research Aircraft has a mechanical control system and a triplex digital Stability and Control Augmentation System (SCAS). The mechanical system is responsible for the safety control system, while the digital SCAS system was to be evaluated through experiments. Functional mock-up tests were carried out to check safety and performance of the total control system using actual system component hardware and simulating aerodynamic and mechanical environmental conditions. This paper describes, as the fundamental process to ensure minimum safety requirements of the system component matching, the mechanical system dynamics test and the total plan for the functional mock-up test. The static and dynamic characteristics of the mechanical control system showed good agreement with the specifications of Japanese Airworthness Standards (equivalent to FAR25) and MIL.
資料番号: NALTR0944000
レポート番号: NAL TR-944
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース(IRDB)(機関リポジトリ)
提供元機関・データベース宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ