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AIAA Infotech @ Aerospace
This paper presents an adaptive control approach for flutter suppression of a performance adaptive aeroelastic wing equipped with a variable camber continuous trailing edge flap design. The adaptive control approach is based on the optimal control modification method augmented to a linear quadratic gaussian optimal control design. A model reduction based on a singular perturbation approach is presented. The control surfaces are subject to relative motion constraints due to the elastomerdoi:10.2514/6.2015-0118 fatcat:hwuyntg2snckzhj65gxoorkrqq