Nonlinear hierarchical control of a quad tilt-wing UAV: An adaptive control approach-Reference-Cited by-同舟云学术

Nonlinear hierarchical control of a quad tilt-wing UAV: An adaptive control approach

Published:2017-02-16 Issue:9 Volume:31 Page:1245-1264
ISSN:0890-6327
Container-title:International Journal of Adaptive Control and Signal Processing
language:en
Short-container-title:Int J Adapt Control Signal Process

Author:

Yildiz Yildiray¹,Unel Mustafa²,Demirel Ahmet Eren²

Affiliation:

1. Department of Mechanical Engineering; Bilkent University; Cankaya, Ankara 06800 Turkey

2. Faculty of Engineering and Natural Sciences; Sabanci University; Tuzla, Istanbul 34956 Turkey

Publisher

Wiley

Subject

Electrical and Electronic Engineering,Signal Processing,Control and Systems Engineering

Reference49 articles.

1. Snyder D The quad tiltrotor: its beginning and evolution Proc. 56th Annual Forum, American Helicopter Society Virginia Beach, Virginia May 2000 48 61

2. Lee J Min B Kim E Autopilot design of tilt-rotor UAV using particle swarm optimization method Proc. International Conference on Control, Automation and Systems Seoul, Korea October 2007 1629 1633

3. Kendoul F Fantoni I Lozano R Modeling and control of a small autonomous aircraft having two tilting rotors Proc. 44th IEEE Conference on Decision and Control, and the European Control Conference Seville, Spain December 2005 1297 1302

4. Dickeson J Miles D Cifdaloz O Wells VL Rodriguez A Robust lpv h-inf gain-scheduled hover-to-cruise conversion for a tilt-wing rotorcraft in the presence of cg variations Proc. 46th IEEE Conference on Decision and Control New Orleans, LA December 2007 2773 2778

5. Muraoka K Okada N Kubo D Quad tilt wing VTOL UAV: aerodynamic characteristics and prototype flight test AIAA Infotech@ Aerospace Conference Seattle, Washington April 2009

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