Mohammad Reza Niknam
Department of Mathematics, Payame Noor University, P.O.Box 19395-3697, Tehran, Iran
[ 1 ] - Finite-time stabilization of satellite quaternion attitude
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 ...
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