DocumentCode :
1950649
Title :
On the stability analysis of a discontinuous quaternion attitude control system
Author :
Septanto, Harry ; Trilaksono, Bambang Riyanto ; Syaichu-Rohman, Arief ; Poetro, Ridanto Eko
Author_Institution :
Sch. of Electr. Eng. & Inf., Inst. Teknol. Bandung, Bandung, Indonesia
fYear :
2012
fDate :
11-12 Sept. 2012
Firstpage :
1
Lastpage :
4
Abstract :
This paper addresses on the stability analysis of the attitude control system using quaternion-based feedback control law that accommodates arcus-cotangent as a discontinuous elements in the control law. Three argumentations of the asymptotically stability guarantee of the attitude control system are proposed that stated in three theorems. The effectiveness of the proposed control law is shown through numerical simulation.
Keywords :
aircraft control; asymptotic stability; attitude control; feedback; numerical analysis; sampled data systems; arcus-cotangent; asymptotic stability analysis; discontinuous quaternion attitude control system; numerical simulation; quaternion-based feedback control law; spacecraft attitude; Asymptotic stability; Attitude control; Feedback control; Lyapunov methods; Quaternions; Space vehicles; Stability analysis; asymptotically stable; attitude control; differensial inclusion; discontinuous differential equation; quaternion feedback;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
System Engineering and Technology (ICSET), 2012 International Conference on
Conference_Location :
Bandung
Print_ISBN :
978-1-4673-2375-8
Type :
conf
DOI :
10.1109/ICSEngT.2012.6339363
Filename :
6339363
Link To Document :
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