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Published in 2020 at "Nonlinear Dynamics"
DOI: 10.1007/s11071-020-05531-8
Abstract: This study investigates the longitudinal flight control problem of air-breathing hypersonic vehicles subject to the asymmetric angle of attack (AoA) constraint. With the help of introduced tangent errors, the proposed control becomes low complexity in…
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Keywords:
asymmetric angle;
angle attack;
control;
constraint ... See more keywords