This paper presents and compares two fuzzy controllers for attitude stabilization of a spacecraft with partially filled fuel tank: a fuzzy controller based on the parallel distributed compensation (PDC) technique and a fuzzy controller based on the linear quadratic regulator. Both controllers are built from the Takagi–Sugeno model of the spacecraft. Using the Lyapunov stability theorem, the fuzzy PDC controller design problem was cast as a minimization problem for the upper bound of control input in the form of linear matrix inequalities. In the end, we compare the efficacy and robustness of each controller via numerical simulations.
Fuzzy Attitude Control of Spacecraft With Fuel Sloshing via Linear Matrix Inequalities
IEEE Transactions on Aerospace and Electronic Systems ; 54 , 5 ; 2526-2536
2018-10-01
1242642 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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