Aircraft Modeling and Simulation

• Tác giả: Ruxandra Mihaela Botez, Teodor Lucian Grigorie, Alejandro Murrieta-Mendoza, Oliviu Sugar-Gabor
• Ngôn ngữ: eng
• ISBN-13: 978-3036532103
• Thông tin xuất bản: Basel : MDPI - Multidisciplinary Digital Publishing Institute, 2022
• Mô tả vật lý: 1 electronic resource (126 p.)
• Bộ sưu tập: Tài liệu truy cập mở
• ID: 232865
• Chủ đề: 1. History of engineering & technology; 2. Technology: general issues

Tóm tắt

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.