DocumentCode
2847273
Title
On tracking for the PVTOL model with bounded feedbacks
Author
Gruszka, A. ; Malisoff, M. ; Mazenc, F.
Author_Institution
Dept. of Math., Louisiana State Univ., Baton Rouge, LA, USA
fYear
2011
fDate
June 29 2011-July 1 2011
Firstpage
1428
Lastpage
1433
Abstract
We study a class of feedback tracking problems for the planar vertical takeoff and landing (PVTOL) aircraft dynamics, which is a benchmark model in aerospace engineering. After a survey of the literature on the model, we construct new feedback stabilizers for the PVTOL tracking dynamics. The novelty of our contribution is in the boundedness of our feedback controllers and their applicability to cases where the velocity measurements may not be available, coupled with the uniform global asymptotic stability and uniform local exponential stability of the closed loop tracking dynamics, the generality of our class of trackable reference trajectories, and the input-to-state stable performance of the closed loop tracking dynamics with respect to actuator errors. Our proofs are based on a new bounded backstepping result. We illustrate our work in a tracking problem along a circle.
Keywords
actuators; aerospace engineering; aircraft control; asymptotic stability; closed loop systems; feedback; tracking; PVTOL aircraft dynamics; PVTOL model; actuator errors; aerospace engineering; bounded feedbacks; closed loop tracking dynamics; feedback controllers; feedback tracking problems; global asymptotic stability; local exponential stability; planar vertical takeoff and landing aircraft dynamics; Actuators; Aircraft; Asymptotic stability; Atmospheric modeling; Backstepping; Tracking loops; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference (ACC), 2011
Conference_Location
San Francisco, CA
ISSN
0743-1619
Print_ISBN
978-1-4577-0080-4
Type
conf
DOI
10.1109/ACC.2011.5990817
Filename
5990817
Link To Document