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Finite-time stabilization of satellite quaternion attitude

Publish Year: 1394
Type: Journal paper
Language: English
View: 163

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Document National Code:

JR_CMDE-3-4_004

Index date: 6 March 2023

Finite-time stabilization of satellite quaternion attitude abstract

In this paper, a finite-time control scheme is presented for stabilization of the satellite chaotic attitude around its equilibrium point when its attitude is confused by a disturbed torque. Controllers and settling time of stabilizaton are obtained, based on the Lyapunov stability theorem and finite-time control scheme. This method is satisfied for any initial condition. Numerical simulations are presented to illustrate the ability and effectiveness of proposed method.

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Finite-time stabilization of satellite quaternion attitude authors

Mohammad Reza Niknam

Department of Mathematics, Payame Noor University, P.O.Box ۱۹۳۹۵-۳۶۹۷, Tehran, Iran

Aghileh Heydari

Department of Mathematics, Payame Noor University, P.O.Box ۱۹۳۹۵-۳۶۹۷, Tehran, Iran