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Robust Attitude Maneuver Control Based on Fuzzy T-S Model

Zhu Liangkuan, Youmin Zhang

Abstract


In this paper, a fuzzy robust control system design method is presented for a three-axis-rotational maneuver and vibration damping of a spacecraft. Firstly, using the lower order model, a robust fuzzy attitude control scheme based on
Takagi-Sugeno (T-S) fuzzy modeling and variable structure control (VSC) technique is provided to design the attitude controller, which accomplishes asymptotic attitude maneuvering in the closed-loop system. Secondly, strain rate feedback control method is presented to suppress the induced vibration actively by using piezoelectric materials as additional sensors and actuators. Numerical simulations are performed to show that rotational maneuver and vibration suppression can be accomplished in spite of the presence of disturbance torque and parameter uncertainty.

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References


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DOI: http://dx.doi.org/10.21535%2FProICIUS.2014.v10.312

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