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