Control Augmentation System Design for Quad-Tilt-Wing Unmanned Aerial Vehicle via Robust Output Regulation Method

Quad-tilt-wing (QTW) configuration is a promising one for airplanes to achieve vertical take-off and landing (VTOL), which has a pair of tandem wings that can tilt from vertical to horizontal positions. This unique configuration allows the aircraft to perform a VTOL as well as fly at high cruising s...

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Veröffentlicht in:	IEEE transactions on aerospace and electronic systems 2017-02, Vol.53 (1), p.357-369
Hauptverfasser:	Anh Tuan Tran, Sakamoto, Noboru, Sato, Masayuki, Muraoka, Koji
Format:	Artikel
Sprache:	eng
Schlagworte:	Actuators Aerodynamic characteristics Aerospace control Aircraft Attitude (inclination) Augmentation Augmentation systems Control Defense industry Military technology Quad-tilt-wing (QTW) robust output regulation Robustness Stability analysis Synthetic aperture sonar Systems design unmanned aerial vehicle (UAV) Unmanned aerial vehicles Vertical landing Vertical orientation vertical take-off and landing (VTOL) Vertical takeoff aircraft Wings (aircraft)
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