Analysis of the Short-Term Dynamics of Morphing Aircraft Caused by Shape Change Based on the Open-Loop Response and the Reachable Set Theory

This work investigates the short-term dynamics caused by shape changes of morphing aircraft. We select a symmetric variable sweep morphing aircraft as the object of study and establish a six-degree-of-freedom multi-loop cascade model, and the coupling between derivative terms is eliminated by matrix...

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Bibliographic Details
Main Authors: Fuming Xia, Bo Jing, Wenfeng Xu
Format: Article
Language:English
Published: MDPI AG 2023-05-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/10/5/448