DocumentCode
1703827
Title
Trajectory control of underactuated hovercraft
Author
Zhao, Jingbo ; Pang, Jinmei
Author_Institution
Dept. of Autom., Qingdao Technol. Univ., Qingdao, China
fYear
2010
Firstpage
3904
Lastpage
3907
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;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Automation (WCICA), 2010 8th World Congress on
Conference_Location
Jinan
Print_ISBN
978-1-4244-6712-9
Type
conf
DOI
10.1109/WCICA.2010.5555061
Filename
5555061
Link To Document