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.
22 Coupled Aeroelastic-Flight Dynamic Framework A P REPRINT N.D
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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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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.