Title
Kinematic And Dynamic Modeling And Control Of A 3-Rotor Aircraft
Abstract
This paper deals with the design of a controller and its implementation in a mini-rotorcraft toy with 3 rotors. A new original low-cost tilt angle sensor is introduced and kinematic and dynamic models are developed and implemented with the aim of developing an autopilot mode to stabilize and maintain hovering flight on demand. The result has to fit into a low-cost microcontroller and run in real-time.
Year
DOI
Venue
2005
10.1109/ROBOT.2005.1570506
2005 IEEE INTERNATIONAL CONFERENCE ON ROBOTICS AND AUTOMATION (ICRA), VOLS 1-4
Keywords
Field
DocType
3-rotor aircraft, hovering flight, Planar Vertical Take Off and Landing (PVTOL), aircraft control and dynamics, low-cost tilt angle sensor
Control theory,Range (aeronautics),Kinematics,Aircraft flight mechanics,Control theory,Control engineering,Flight simulator,Rotor (electric),Microcontroller,Autopilot,Engineering
Conference
Volume
Issue
ISSN
2005
1
1050-4729
Citations 
PageRank 
References 
3
0.55
5
Authors
3
Name
Order
Citations
PageRank
Philippe Rongier130.55
Erwann Lavarec230.55
F. Pierrot347992.02