Abstract
This work addresses the robust neural direct control of hypersonics flight vehicle (HFV) under dynamics uncertainty and actuator saturation. The controller is constructed with robust control and neural control. To deal with the actuator saturation, a Gaussian error function is employed to express the effect. The dynamic surface control (DSC) is studied to remove the explosion of the complexity by using a nonlinear adaptive filter. The simulation tested on the hypersonic vehicle control-oriented model (COM) shows the effectiveness of the control design.
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