@techreport{oai:jaxa.repo.nii.ac.jp:00044141,
 author = {田中, 敬司 and TANAKA, Keiji},
 month = {Dec},
 note = {A basic design concept of a flight director system for the NAL STOL Research Air-craft “ASUKA” is proposed and evaluated with the help of a CAD (Computer Aided Design) tool for control system synthesis. The flight director system designed for backside operations during the approach and landing phase of ASUKA has three commands presented by one integrated symbol : pitch command for speed control, flight path command for Flight Path Control lever manipulation, and bank command for lateral control. In determining the flight-director dynamics, closed loop analysis was conducted of pilot, aircraft, control systems, and navigational sites, as well as the flight director system itself. Dialogical communications with the CAD system enabled the quick and simple determination of the dynamics. Dynamics and constants of the flight director system confirmed by the present study form a basis for future design of flight director systems for USB type aircraft., 資料番号: NALTM0558000, レポート番号: NAL TM-558},
 title = {STOL実験機用フライト・ディレクタ・システムの基礎設計},
 year = {1986}
}