DocumentCode :
3601434
Title :
Global Exponential Attitude Tracking Controls on {mathsf {SO}}({mathsf 3})
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 :
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