@techreport{oai:jaxa.repo.nii.ac.jp:00043831,
 author = {堀川, 勇壮 and 小川, 鑛一 and 永安, 正彦 and HORIKAWA, Yuso and OGAWA, Koichi and NAGAYASU, Masahiko},
 month = {Oct},
 note = {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},
 title = {自動着陸研究用テスト・リグについて},
 year = {1973}
}