Finite-time stabilization of satellite quaternion attitude
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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.
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finite-time stabilization of satellite quaternion attitude
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Journal title
volume 3 issue 4
pages 274- 283
publication date 2015-10-01
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