Aircraft Modeling and Simulation

• Pubblicazione: Basel, : MDPI - Multidisciplinary Digital Publishing Institute, 2022
• Descrizione fisica: 1 electronic resource (126 pages)
• Soggetto topico: Technology - History; Engineering - History
• Soggetto non controllato: tailless aircraft; nonlinear dynamic inversion; disturbance observer; anti-windup; flight tests; wind tunnel; morphing airfoil optimization; parameterization; PSO; aerodynamic performance; computational fluid dynamics; turbulence modeling; flat plate flow; backward-facing step flow; airfoil flow; cascade flow; adaptive structures; FE modeling; stress analysis; loads assessment; landing gear dynamics; drop impact; oleo-pneumatic shock absorber; ground loads; spin-up; spring-back
• Persona (resp. second.): GrigorieTeodor Lucian; Sugar-GaborOliviu; Murrieta-MendozaAlejandro; BotezRuxandra Mihaela
• Sommario/riassunto: Various aerodynamics, structural dynamics, and control design and experimental studies are presented with the aim of advancing green and morphing aircraft research. The results obtained with an in-house CFD code are compared and validated with those of two NASA codes. The aerodynamical model of the UAS-S45 morphing wing as well as the structural model of a morphing winglet are presented. A new design methodology for oleo-pneumatic landing gear drop impact dynamics is presented as well as its experimental validation. The design of a nonlinear dynamic inversion (NDI)-based disturbance rejection control on a tailless aircraft is presented, including its validation using wind tunnel tests.
• Titolo autorizzato: Aircraft Modeling and Simulation
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910557619903321
• Lo trovi qui: Univ. Federico II