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. R. and Heydari, A. (2015). Finite-time stabilization of satellite quaternion attitude. Computational Methods for Differential Equations, 3(4), 274-283.
MLA
Niknam, M. R. , and Heydari, A. . "Finite-time stabilization of satellite quaternion attitude", Computational Methods for Differential Equations, 3, 4, 2015, 274-283.
HARVARD
Niknam, M. R., Heydari, A. (2015). 'Finite-time stabilization of satellite quaternion attitude', Computational Methods for Differential Equations, 3(4), pp. 274-283.
CHICAGO
M. R. Niknam and A. Heydari, "Finite-time stabilization of satellite quaternion attitude," Computational Methods for Differential Equations, 3 4 (2015): 274-283,
VANCOUVER
Niknam, M. R., Heydari, A. Finite-time stabilization of satellite quaternion attitude. Computational Methods for Differential Equations, 2015; 3(4): 274-283.
)
