@techreport{oai:jaxa.repo.nii.ac.jp:00043833,
 author = {小川, 鉱一 and 堀川, 勇壮 and 渡辺, 顕 and 永安, 正彦 and OGAWA, Koichi and HORIKAWA, Yuso and WATANABE, Akira and NAGAYASU, Masahiko},
 month = {Nov},
 note = {This paper describes an experimental and fundamental studies of multiplex elevator servo system for an automatic landing system. This multiplex system is a non-disconnecting redundant triplex system without any failure detectors, and each subsystem consists of vertical gyro, rate gyro, autopilot computer and control surface actuator. The performance tests and failure analysis of this triplex system have been conducted, using a rig test stand which has control rigs and control apparatus of an experimental aircraft. From the results of failure analysis, the fundamental design data about the non- disconnecting redundant system were obtained. Moreover it was cleared that even if one channel in the system failed, the multiplex system works well but generates a small error of the control output., 資料番号: NALTM0250000, レポート番号: NAL TM-250},
 title = {自動着陸用多重サーボ機構について},
 year = {1973}
}