Aranda Almansa, Joaquín2024-05-202024-05-202007-11-12https://hdl.handle.net/20.500.14468/15622Over the last two decades or so, control researchers have begun to apply alternative methodologies to flight control design. One alternative is variously called non-linear dynamic inversion or feedback linearization. The purpose of dynamic inversion is to develop a feedback control law that linearizes the plant response to commands. Simple controllers can then be designed. With dynamic inversion, a non-linear control law is designed which globally reduces the dynamics of selected controlled variables to integrators. A closed loop system is then designed to make the controlled variables exhibit specified command responses while satisfying the usual disturbances response and robustness requirements for the overall system and the various physical limitations of the aircraft’s control effectors.enAtribución-NoComercial-SinDerivadas 4.0 Internacionalcapítulo de libroROBUSTCONTROLTECHNIQUESNon LinearDynamicInversionTechnique