Electronic Resource

Aircraft Modeling and Simulation

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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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Detail Information

Series Title

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Call Number

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Publisher

Basel : MDPI - Multidisciplinary Digital Publishing Institute., 2022

Collation

126 hlm; ill., lamp.,

Language

English

ISBN/ISSN

9783036532110 Publisher

Classification

NONE

Content Type

text

Media Type

computer

Carrier Type

online resource

Edition

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Subject(s)

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Specific Detail Info

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Statement of Responsibility

Botez, Ruxandra Mihaela (editor) Grigorie, Teodor Lucian (editor) Sugar-Gabor, Oliviu (editor) Murrieta-Mendoza, Alejandro (editor)

Other Information

Cataloger

ida

Source

https://directory.doabooks.org/handle/20.500.12854/79648

Validator

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Digital Object Identifier (DOI)

10.3390/books978-3-0365-3211-0

Journal Volume

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Journal Issue

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Subtitle

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Parallel Title

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