Paper Info
Title
Global configuration stabilization for the VTOL aircraft with strong input coupling
Abstract
Trajectory tracking and configuration stabilization for the vertical takeoff and landing (VTOL) aircraft has been so far considered in the literature only in the presence of a slight (or zero) input coupling (i.e., for a small ). In this note, our main contribution is to address global con- figuration stabilization for the VTOL aircraft with a strong input coupling using a smooth static state feedback. In addition, the differentially flat out- puts for the VTOL aircraft are automatically obtained as a by-product of applying a decoupling change of coordinates.
Year
DOI
Venue
2002
10.1109/TAC.2002.804457
IEEE Trans. Automat. Contr.
Keywords
DocType
Volume
Aircraft,State feedback,Backstepping,Control systems,Control design,Automatic control,Trajectory,Vehicle dynamics,Aerodynamics,Linear approximation
Journal
47
Issue
ISSN
ISBN
11
0018-9286
0-7803-6638-7
Citations 
PageRank 
References 
49
4.74
2
Authors
1
Name
Order
Citations
PageRank
Reza Olfati-Saber18066549.43