その他

基本情報

氏名 箕原 辰夫
氏名(カナ) ミノハラ タツオ
氏名(英語) MINOHARA, Tatsuo
所属 政策情報学部
職名 教授
researchmap研究者コード
researchmap機関

翻訳書、学会発表、講演、作品等の名称

Display System for Control Configured Vehicle

単・共の別

単著

発行又は発表の年月

200410

発表学会等の名称

Proceedings of 23rd Digital Avionics Systems Conference, Salt lake city

概要

In a helicopter or an airplane which has enhanced maneuverability by using active control technology, its nose vector can be directed at a wide angle with its velocity vector. Especially, the maneuvers of an airplane which has widely enhanced maneuverability, such as X-31 and Su-27 should be focused to rather than an usual CCV (Control Configured Vehicle) plane, such as X-29 and F-16 CCV.  Also in a space plane, such differences of angles are usually controlled and precisely used when docking or landing to the target station. Those angles of the vehicle should be indicated against the velocity vector and also against the target.  In addition to the indication of the angles, indicators of speeds and relative position against the target are required to direct side force control and direct lift control. In this paper, a display system in which fuselage pointing,  translation movements, and direct forces are indicated is proposed. Those indications will improve the recognition of maneuver for a pilot. This display system is currently virtually implemented in a simple flight simulator software.

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