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- W2127804745 abstract "Wing rock is a rolling motion characterized by self-excited oscillations which appears at high angles of attack in aircraft with highly-swept wings. In this paper an analyti- cal model describing this phenomenon is presented for simple wing and wing-fuselage layouts. The parameters of the model were derived through numerical tting of ex- perimental data. For both cases an L1 adaptive controller is applied to suppress the wing rock motion for dierent angles of attack and initial conditions. Adaptation ca- pability is assessed testing the controller action on a model subjected to parametric disturbances. The controller can suppress the motion with satisfactory performance for both congurations, even when disturbed" @default.
- W2127804745 created "2016-06-24" @default.
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- W2127804745 date "2012-11-01" @default.
- W2127804745 modified "2023-10-05" @default.
- W2127804745 title "Performance Evaluation of an L1 Adaptive Controller for Wing-Body Rock Suppression" @default.
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- W2127804745 doi "https://doi.org/10.2514/1.57595" @default.
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