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To circumvent the non-minimum phase behavior in a hypersonic flight vehicle, an asymptotic flight tracking controller is investigated in this work. When the elevator is the only control surface available for the altitude dynamics, the hypersonic vehicle model exhibits unstable zero dynamics, preventing the application of standard inversion-based control techniques. The standard output regulation theory...
The standard output regulation theorem is utilized to construct a nonlinear flight tracking controller for a hypersonic vehicle in presence of non-minimum phase dynamic in the paper. When the elevator is chosen as the only control surface, the hypersonic vehicle model exhibits unstable hyperbolic zero-dynamics, preventing the application of standard inversion-based control technique. The standard...
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