DocumentCode
3601434
Title
Global Exponential Attitude Tracking Controls on
Author
Taeyoung Lee
Author_Institution
Dept. of Mech. & Aerosp. Eng., George Washington Univ., Washington, DC, USA
Volume
60
Issue
10
fYear
2015
Firstpage
2837
Lastpage
2842
Abstract
This technical note presents four types of tracking control systems for the attitude dynamics of a rigid body. First, a smooth control system is constructed to follow a given desired attitude trajectory, while guaranteeing almost semi-global exponential stability. It is generalized to achieve global exponential stability by using a hybrid control scheme based on multiple configuration error functions. They are further extended to obtain robustness with respect to a fixed disturbance using an integral term. The resulting robust, global exponential stability for attitude tracking is the unique contribution of this technical note.
Keywords
aircraft control; asymptotic stability; attitude control; trajectory control; attitude dynamics; attitude tracking; attitude trajectory; fixed disturbance; global exponential attitude tracking controls; hybrid control scheme; integral term; multiple configuration error functions; rigid body; semiglobal exponential stability; smooth control system; tracking control systems; Asymptotic stability; Attitude control; Control theory; Robustness; Stability; Switches; Attitude control; geometric control; hybrid systems; special orthogonal group;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/TAC.2015.2407452
Filename
7050256
Link To Document