Aircraft Modeling and Simulation
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...
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| 其他作者: | , , , |
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| 格式: | 本书章节 |
| 出版: |
Basel
MDPI - Multidisciplinary Digital Publishing Institute
2022
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| 在线阅读: | Get Fullteks DOAB: description of the publication |
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| 总结: | 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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| 实物描述: | 1 electronic resource (126 p.) |
| ISBN: | books978-3-0365-3211-0 9783036532103 9783036532110 |
| 访问: | Open Access |