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In this paper, the finite-time fault tolerant control (FTC) of attitude stabilization is developed for attitude dynamical system of a hypersonic unmanned aerial vehicle (UAV) with actuator loss-of-effectiveness (LOE) fault. First, the hypersonic UAV non-linear attitude dynamics are described. A finite-time controller is designed on the basis of nonsingular terminal sliding mode (NTSM) control technique...
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