@techreport{oai:jaxa.repo.nii.ac.jp:00045231,
 author = {STOLプロジェクト推進本部実験機開発室操縦システム技術開発チーム and 内田, 忠夫 and 多田, 章 and 岡田, 典秋 and 大和, 裕幸 and 小川, 敏雄 and STOL Aircraft Project Group and UCHIDA, Tadao and TADA, Akira and OKADA, Noriaki and YAMATO, Hiroyuki and OGAWA, Toshio},
 month = {Apr},
 note = {In this paper the functional mockup test of the flight control system of ASKA with the stability and control augmentation systems is described. The tests made included software verification, simulated failure effects testing, closed loop test, and piloted simulation test. The results showed that the functions and performance of the control system were satisfactory for flight safety of ASKA., 資料番号: NALTR0972000, レポート番号: NAL TR-972},
 title = {The Functional Mock-up Test of the Flight Control System of the NAL QSTOL Research Aircraft “ASKA”},
 year = {1988}
}