DocumentCode
189443
Title
Trajectory-tracking control design for an under-actuated quadrotor
Author
Hao Nguyen Dang ; Mohamed, B. ; Rafaralahy, Hugues
Author_Institution
Res. Centre for Autom. Control (CRAN), Lorraine Univ., Vandoeuvre, France
fYear
2014
fDate
24-27 June 2014
Firstpage
1765
Lastpage
1770
Abstract
Path-tracking and trajectory-tracking for a quadrotor are basic tasks when solving the motion control. The difference between path-tracking and trajectory-tracking is that the reference trajectory is generated by a suitable virtual quadrotor whereas the reference path is not required to be generated by a virtual quadrotor. In this paper, we propose a trajectory-tracking controller for an underactuated quadrotor. A new change in describing the dynamics of the quadrotor is presented from which we can determine the direction of motion of the quadrotor in the horizontal plane through its gravity center. After this change, we can separate the dynamics of the system into three sub-groups then combine with a coordinate transformation to design control for the quadrotor. The controller synthesis is based on Lyapunov direct method and the backstepping technique. Simulations illustrate the effectiveness of the proposed controller.
Keywords
Lyapunov methods; aircraft control; control system synthesis; gravity; helicopters; motion control; path planning; trajectory control; vehicle dynamics; Lyapunov direct method; backstepping technique; controller synthesis; coordinate transformation; gravity center; motion control; path-tracking; quadrotor control design; quadrotor dynamics; quadrotor motion direction; reference path; reference trajectory; system dynamics; trajectory-tracking control design; under-actuated quadrotor; underactuated quadrotor; virtual quadrotor; Actuators; Backstepping; Control design; Dynamics; Gravity; Lyapunov methods; Propellers;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (ECC), 2014 European
Conference_Location
Strasbourg
Print_ISBN
978-3-9524269-1-3
Type
conf
DOI
10.1109/ECC.2014.6862517
Filename
6862517
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