Title :
Trajectory control of underactuated hovercraft
Author :
Zhao, Jingbo ; Pang, Jinmei
Author_Institution :
Dept. of Autom., Qingdao Technol. Univ., Qingdao, China
Abstract :
The track-keeping control of a hovercraft is considered. The hovercraft dynamic model is nonlinear and underactuated. In this paper, a control law is established that drives the sway velocity error and heading error to zero. Simulation tests are carried out for illustrating the effectiveness of the proposed method.
Keywords :
aircraft control; position control; control law; hovercraft dynamic model; sway velocity error; track-keeping control; trajectory control; underactuated hovercraft; hovercraft; track-keeping; underactuated system;
Conference_Titel :
Intelligent Control and Automation (WCICA), 2010 8th World Congress on
Conference_Location :
Jinan
Print_ISBN :
978-1-4244-6712-9
DOI :
10.1109/WCICA.2010.5555061
