[HTML][HTML] Design, modeling, and control of morphing aircraft: A review

CHU Lingling, LI Qi, GU Feng, DU Xintian… - Chinese journal of …, 2022 - Elsevier
A morphing aircraft can adapt its configuration to suit different types of tasks, which is also an
important requirement of Unmanned Aerial Vehicles (UAV). The successful development of …

Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics

J Murua, R Palacios, JMR Graham - Progress in Aerospace Sciences, 2012 - Elsevier
The unsteady vortex-lattice method provides a medium-fidelity tool for the prediction of non-
stationary aerodynamic loads in low-speed, but high-Reynolds-number, attached flow …

Birds can transition between stable and unstable states via wing morphing

C Harvey, VB Baliga, JCM Wong, DL Altshuler… - Nature, 2022 - nature.com
Birds morph their wing shape to accomplish extraordinary manoeuvres,,–, which are
governed by avian-specific equations of motion. Solving these equations requires …

Morphing control of a new bionic morphing UAV with deep reinforcement learning

D Xu, Z Hui, Y Liu, G Chen - Aerospace science and technology, 2019 - Elsevier
With rapid development of aviation technology, materials science and artificial intelligence,
aircraft design is pursuing higher requirements both in civil and military fields. The new …

[HTML][HTML] Gain self-scheduled H∞ control for morphing aircraft in the wing transition process based on an LPV model

T Yue, L Wang, J Ai - Chinese journal of aeronautics, 2013 - Elsevier
This article investigates gain self-scheduled H∞ robust control system design for a tailless
folding-wing morphing aircraft in the wing shape varying process. During the wing morphing …

Flight dynamic modeling and control for a telescopic wing morphing aircraft via asymmetric wing morphing

T Yue, X Zhang, L Wang, J Ai - Aerospace Science and Technology, 2017 - Elsevier
In this paper, a sliding mode flight controller is formulated in order to enhance the lateral
maneuverability for a tailless telescopic wing morphing aircraft by using additional …

Multifidelity modeling of deployable wings: Multibody dynamic simulation and wind tunnel experiment

K Otsuka, Y Wang, K Fujita, H Nagai, K Makihara - AIAA journal, 2019 - arc.aiaa.org
Slender deployable wings have attracted interest for use in Mars, Titan, and high-altitude
flights. Such wings are composed of multiple bodies connected by hinge joints and can be …

[HTML][HTML] 一种变体飞行器的动力学建模与动态特性分析

张杰, 吴森堂 - 北京航空航天大学学报, 2015 - bhxb.buaa.edu.cn
对可变展长, 可变后掠角的变体飞行器物理模型进行了简化, 基于Kane 方法,
将变体运动假设为已知的可控输入, 利用约束方程来表示机翼的变形运动, 选取飞行器位移运动 …

A flight mechanics-centric review of bird-scale flapping flight

AA Paranjape, MR Dorothy, SJ Chung… - International Journal of …, 2012 - koreascience.kr
This paper reviews the flight mechanics and control of birds and bird-size aircraft. It is
intended to fill a niche in the current survey literature which focuses primarily on the …

Adaptive neural control based on high order integral chained differentiator for morphing aircraft

Z Wu, J Lu, J Rajput, J Shi, W Ma - Mathematical Problems in …, 2015 - Wiley Online Library
This paper presents an adaptive neural control for the longitudinal dynamics of a morphing
aircraft. Based on the functional decomposition, it is reasonable to decompose the …