Analysis of the Short-Term Dynamics of Morphing Aircraft Caused by Shape Change Based on the Open-Loop Response and the Reachable Set Theory
Author:
Affiliation:
1. Graduate College, Air Force Engineering University, Xi’an 710038, China
2. Beijing Electro-Mechanical Engineering Institute, Beijing 100074, China
3. Aeronautics Engineering College, Air Force Engineering University, Xi’an 710038, China
Abstract
Funder
14th Five-Year Plan equipment pre-research and common technology project
Publisher
MDPI AG
Subject
Aerospace Engineering
Link
https://www.mdpi.com/2226-4310/10/5/448/pdf
Reference24 articles.
1. A review of modelling and analysis of morphing wings;Li;Prog. Aerosp. Sci.,2018
2. A Review of Morphing Aircraft;Barbarino;J. Intell. Mater. Syst. Struct.,2011
3. Modeling and flight control of large-scale morphing aircraft;Seigler;J. Aircr.,2007
4. Xu, W.F., Li, Y.H., Pei, B.B., and Yu, Z.L. (2023). A Nonlinear Programming-Based Morphing Strategy for a Variable-Sweep Morphing Aircraft Aiming at Optimizing the Cruising Efficiency. Aerospace, 10.
5. A study of morphing aircraft on morphing rules along trajectory;Chen;Chin. J. Aeronaut.,2021
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