日本航空宇宙学会誌
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
T-2 CCVの Pilot-Induced Oscillation (PIO) 特性とその改善
菅野 秀樹片柳 亮二
著者情報
ジャーナル フリー

1995 年 43 巻 498 号 p. 405-414

詳細
抄録

Pilot-Induced Oscillation (PIO) was encountered in the company flight test of the T-2CCV research vehicle. The main cause of the roll PIO was due to unexpected large pilot input and to increased delay of the aircraft response by its large pilot input. The delay of roll response has much difference between with large input and with small input. That is why the flight control system falls into nonlinear system by actuator rate limit in case of controlling the aircraft with large pilot input. This paper shows analysis of the characteristics of the PIO and its improvement.

著者関連情報
© The Japan Society for Aeronautical and Space Sciences
前の記事 次の記事
feedback
Top