並列タイトル等Test Rig for Automatic Landing System Study
タイトル（掲載誌）航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory
一般注記Studies on hardwares of automatic landing system, as a part of automatic landing system study programs, have been conducted at National Aerospace Laboratory. A test rig for the study on the hardwares has been designed and constructed. The test rig is a ground test equipment for evaluating the. automatic flight control system including actual hardwares and human factors of a pilot. The testing hardwares, such as servo actuators, servo amplifiers, auto-land computers and control pannels so on, are equipped on the test rig and tested in a simulated flight condition with an analog computer. The test rig has actual control systems of experimental aircraft, which is Beechcraft Queen Air Model 65, such as elevator control system, aileron control system, rudder cont- rol system, trim controls, and engine throttle control system. And each of the control systems consists of control rigs, pulleies, control load which is simulated an aerodynamic load and control wheel or pedal. In this paper, the design, construction and performance of the test rig are reported here.
資料番号: NALTM0248000
レポート番号: NAL TM-248
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43831&item_no=1&attribute_id=31&file_no=1
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