B Yan, P Dai, R Liu, M Xing, S Liu - Aerospace Science and Technology, 2019 - Elsevier
In this paper, a novel and more explicit longitudinal model of a wing-sweep morphing aircraft is proposed, accounting for the variations in aerodynamics, mass and inertial properties. In …
W Xu, Y Li, M Lv, B Pei - Aerospace Science and Technology, 2022 - Elsevier
This paper investigates the problems of modeling and control of the morphing aircraft. Henceforth, a nonlinear dynamic model of a wing-sweep morphing aircraft is first …
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 …
Z Wu, J Lu, Q Zhou, J Shi - Nonlinear Dynamics, 2017 - Springer
In this paper, a barrier Lyapunov function-based adaptive neural dynamic surface control approach is proposed for morphing aircraft subject to unknown parameters and input–output …
X Wang, T Mkhoyan, I Mkhoyan… - Journal of Guidance …, 2021 - arc.aiaa.org
This paper deals with the simultaneous gust and maneuver load alleviation problem of a seamless active morphing wing. The incremental nonlinear dynamic inversion with …
This paper reviews the various control algorithms and strategies used for fixed-wing morphing aircraft applications. It is evident from the literature that the development of control …
T Yue, L Wang, J Ai - Journal of aircraft, 2013 - arc.aiaa.org
The purpose of this paper is to present linear parameter varying modeling and simulation of a folding-wing morphing aircraft in the wing-folding process. Morphing aircraft can alter the …
B Yan, Y Li, P Dai, S Liu - Journal of Aerospace Engineering, 2019 - ascelibrary.org
In this paper, a longitudinal dynamic model of a variable-sweep-wing morphing aircraft is proposed based on the Firebee unmanned aerial vehicle (UAV), accounting for changes in …
W Jiang, K Wu, Z Wang, Y Wang - Aerospace Science and Technology, 2020 - Elsevier
This paper addresses the gain-scheduled output feedback control for morphing aircraft (MA) in full envelope using switching polytopic linear parameter-varying (SPLPV) theory. The …