H-infinity controllers synthesized on 8-9 DOF reduced-order models of nonlinear flexible aircraft can robustly alleviate gust loads on the full nonlinear system.
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3 Pith papers cite this work. Polarity classification is still indexing.
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MRAC with Lyapunov stability is formulated for gust load alleviation in nonlinear aeroelastic systems, demonstrating superior performance over H-infinity control in UAV gust and turbulence tests.
A self-contained state-space framework couples geometrically-exact beam theory, Theodorsen aerodynamics with indicial gust functions, and quaternion flight dynamics for free-flying flexible aircraft encountering atmospheric gusts.
citing papers explorer
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H Infinity Robust Control for Gust Load Alleviation of Geometrically Nonlinear Flexible Aircraft
H-infinity controllers synthesized on 8-9 DOF reduced-order models of nonlinear flexible aircraft can robustly alleviate gust loads on the full nonlinear system.
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Model Reference Adaptive Control For Gust Load Allevation of Nonlinear Aeroelastic
MRAC with Lyapunov stability is formulated for gust load alleviation in nonlinear aeroelastic systems, demonstrating superior performance over H-infinity control in UAV gust and turbulence tests.
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A coupled Aeroelastic-Flight Dynamic Framework for Free-Flying Flexible Aircraft with Gust Interactions
A self-contained state-space framework couples geometrically-exact beam theory, Theodorsen aerodynamics with indicial gust functions, and quaternion flight dynamics for free-flying flexible aircraft encountering atmospheric gusts.