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Wang, Z. (author), Peeters, D.M.J. (author), De Breuker, R. (author)In the structural design of aircraft wings, aeroelastic tailoring is used to control the aeroelastic deformation to improve the aerostructural performance by making use of directional stiffness. Recently, tow-steered composites, where the fibre angles continuously vary within each ply, have been proven to have the potential to further expand...journal article 2021
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Mkhoyan, T. (author), Wang, Xuerui (author), de Visser, C.C. (author), De Breuker, R. (author)The advancements made in aircraft control methodology and the tendency towards increasingly lighter aircraft structures open the opportunity to higher structural performance and aerodynamic efficiency. However, with the reduction of structure weight, the structure stiffness reduces typically, which makes the structure more susceptible to...other 2020
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Mkhoyan, T. (author), Stuber, V.L. (author), Nazeer, N. (author), De Breuker, R. (author), Groves, R.M. (author), Groen, W.A. (author), van der Zwaag, S. (author), Sodja, J. (author), Wang, X. (author)PowerPoint presentationother 2020
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Wang, Xuerui (author), van Kampen, E. (author), Chu, Q. P. (author), De Breuker, R. (author)This paper designs an incremental nonlinear dynamic inversion control law for free-flying flexible aircraft, which can regulate rigid-body motions, alleviate gust loads, reduce the wing root bending moment, and suppress elastic modes. By fully exploring the sensor measurements, the model dependency of the proposed control law can be reduced...journal article 2019
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Natella, M. (author), Wang, Xuerui (author), De Breuker, R. (author)This paper presents a unified framework for aeroelastic tailoring of free-flying aircraft with composite wings. A continuous-time state-space model is used to describe the flow. The 3D composite wing structures is condensed into a Timoshenko beam model by means of a cross-sectional modeler. The aerodynamic and structural models are closely...conference paper 2018
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Wang, Xuerui (author), van Kampen, E. (author), Chu, Q. P. (author), De Breuker, R. (author)In this paper, an Incremental Nonlinear Dynamic Inversion (INDI) controller is<br/>developed for the flexible aircraft gust load alleviation (GLA) problem. First, a flexible aircraft model captures both inertia and aerodynamic coupling effects between flight dynamics and structural vibration dynamics is presented. Then an INDI GLA controller is...conference paper 2018
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