DocumentCode
189458
Title
On the finite-time stabilizability of triangular control systems. Applications
Author
Jammazi, Chaker
Author_Institution
Dept. de Math., Univ. de Carthage, Tunis, Tunisia
fYear
2014
fDate
24-27 June 2014
Firstpage
1422
Lastpage
1427
Abstract
In this paper an extension of several sufficient conditions for finite-time stability of triangular systems are provided. We apply our conditions to show that the angular momentum equations, for a rigid spacecraft with two controls, is finite-time stabilizable. This allows to conclude the partial guidance of several under-actuated systems as the X4 flyer.
Keywords
aerospace control; space vehicles; stability; X4 flyer; angular momentum equations; finite-time stabilizability; partial guidance; rigid spacecraft; triangular control systems; under-actuated systems; Asymptotic stability; Lyapunov methods; Manifolds; Stability analysis; State feedback; Thermal stability;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (ECC), 2014 European
Conference_Location
Strasbourg
Print_ISBN
978-3-9524269-1-3
Type
conf
DOI
10.1109/ECC.2014.6862525
Filename
6862525
Link To Document