Department of Mathematics, Payame Noor University, P.O.Box 19395-3697, Tehran, Iran
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.
Niknam, M., Heydari, A. (2015). Finite-time stabilization of satellite quaternion attitude. Computational Methods for Differential Equations, 3(4), 274-283.
MLA
Mohammad Reza Niknam; Aghileh Heydari. "Finite-time stabilization of satellite quaternion attitude". Computational Methods for Differential Equations, 3, 4, 2015, 274-283.
HARVARD
Niknam, M., Heydari, A. (2015). 'Finite-time stabilization of satellite quaternion attitude', Computational Methods for Differential Equations, 3(4), pp. 274-283.
VANCOUVER
Niknam, M., Heydari, A. Finite-time stabilization of satellite quaternion attitude. Computational Methods for Differential Equations, 2015; 3(4): 274-283.
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