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
Aircraft Modeling and Simulation
2022
1 Online-Ressource (126 p.)
Book
Electronic Resource
Unknown
nonlinear dynamic inversion , airfoil flow , History of engineering & technology , aerodynamic performance , stress analysis , computational fluid dynamics , backward-facing step flow , adaptive structures , wind tunnel , spin-up , Technology: general issues , landing gear dynamics , tailless aircraft , disturbance observer , n/a , turbulence modeling , oleo-pneumatic shock absorber , PSO , FE modeling , drop impact , parameterization , loads assessment , anti-windup , flight tests , flat plate flow , cascade flow , morphing airfoil optimization , ground loads , spring-back
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