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The command filter based robust nonlinear controller is designed for the longitudinal dynamics of a generic hypersonic aircraft in presence of parametric model uncertainty and magnitude constraints on the states and actuators. The functional subsystems are transformed into the linearly parameterized form and the controller is proposed based on dynamic inversion and adaptive gain. Since the dynamics...
In this paper, the robust adaptive controller is investigated for the longitudinal dynamics of a generic hypersonic aircraft in presence of uncertain parameters. The control-oriented model is adopted for design and stability analysis. By transferring the altitude command into the flight path angle trajectory, the dynamics are decomposed into velocity and attitude subsystems. Furthermore, the subsystems...
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