Attitude Control of Quad Rotors QTW-UAV with Tilt Wing Mechanism

• Published in: Nihon Kikai Gakkai ronbunshū. C Vol. 19; no. 7; pp. 2012 - 2019
• Main Authors: Suzuki, Satoshi, Ren, Zhijia, Horita, Yoshikazu, Nonami, Kenzo, Kimura, Gaku, Bando, Toshio, Hirabayashi, Daisuke, Furuya, Mituhiro, Yasuda, Kenta
• Format: Journal Article
• Language: Japanese
• Published: 01.07.2007

In this paper, we propose the autonomous attitude control of Quad Tilt Wing (QTW) -UAV. QTW-UAV can realize the vertical takeoff and landing, and hovering flight that seems to be the helicopter, and the high cruising speed that seems to be the fixed-wing aircraft by changing an angle of a rotors and...