Theis, JulianJulianTheisPfifer, HaraldHaraldPfiferBalas, GaryGaryBalasWerner, HerbertHerbertWerner2020-09-242020-09-242015-07Proceedings of the American Control Conference (2015-July): 7171927 3830-3835 (2015-07)http://hdl.handle.net/11420/7388A systematic design procedure suited to integrate rigid body and aeroelastic control objectives within the mixed sensitivity framework is proposed for a two-degrees-of-freedom control configuration. It is based on a modal representation and combines stability augmentation, structural mode control and maneuver demand in a single linear parameter-varying (LPV) controller. To demonstrate applicability, an integrated flight control system is designed for the nonlinear model of a large flexible aircraft. The integrated controller is shown to greatly reduce structural vibrations while maintaining handling qualities and robustness margins of a conventional controller.en0743-1619201538303835Conference Paper10.1109/ACC.2015.7171927Other