finite-time stabilization of satellite quaternion attitude
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abstract
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 presented to illustrate the ability andeffectiveness of proposed method.
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Journal title:
computational methods for differential equationsجلد ۳، شماره ۴، صفحات ۲۷۴-۲۸۳
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