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- Publisher: MDPI AG
- ISBN-10: 3036532102
- ISBN-13: 9783036532103
- Format: 17 x 24.4 x 1.3 cm, hardcover
- Language: English
- SAVE -10% with code: EXTRA
Aircraft Modeling and Simulation (e-book) (used book) | bookbook.eu
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Description
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.
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- Publisher: MDPI AG
- ISBN-10: 3036532102
- ISBN-13: 9783036532103
- Format: 17 x 24.4 x 1.3 cm, hardcover
- Language: English English
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.
Reviews