Finite-time stabilization of satellite quaternion attitude

نویسندگان

  • Aghileh Heydari Department of Mathematics, Payame Noor University, P.O.Box 19395-3697, Tehran, Iran
چکیده مقاله:

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

in this paper, a finite-time control scheme is presented for stabilization ofthe satellite chaotic attitude around its equilibrium point whenits attitude is confused by a disturbed torque. controllers and settling timeof stabilizaton are obtained, based on the lyapunov stability theoremand finite-time control scheme. this method is satisfied for any initial condition.numerical simulations are ...

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عنوان ژورنال

دوره 3  شماره 4

صفحات  274- 283

تاریخ انتشار 2015-10-01

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