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Nonlinear incremental control for flexible aircraft trajectory tracking and load alleviation

Autor: Tigran Mkhoyan, Xuerui Wang, R. De Breuker

Publikováno v: AIAA Scitech 2021 Forum: 11–15 & 19–21 January 2021, Virtual Event
AIAA Scitech 2021 Forum
Journal of Guidance, Control, and Dynamics: devoted to the technology of dynamics and control, 45(1)

This paper proposes a nonlinear control architecture for flexible aircraft simultaneous trajectory tracking and load alleviation. By exploiting the control redundancy, the gust and maneuver loads are alleviated without degrading the rigid-body comman

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f59cc5070dc19660e6d4de8dfed19705
http://resolver.tudelft.nl/uuid:b24db4db-a89b-492f-92ea-2be2f397dcd3

Developing the Model Reduction Framework in High Frame Rate Visual Tracking Environment

Autor: C.C. de Visser, Tigran Mkhoyan, Abdul Abdul Rozak Rivai Fassah, R. De Breuker

Publikováno v: AIAA Scitech 2021 Forum: 11–15 & 19–21 January 2021, Virtual Event
AIAA Scitech 2021 Forum

The developments in the field of aerospace materials and structures allow the more light weight air vehicles. However, the aircraft body, particularly wing, can deform more appreciably due to the occurrence of flow separation and flutter. Therefore,

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5f6cd0b18931c39d648650b9ae1d78bf
http://resolver.tudelft.nl/uuid:8acded3a-2d77-4577-9c12-72c680a7c355

Design and testing of aeroelastically tailored composite wing under fatigue and gust loading including effect of fatigue on aeroelastic performance

Autor: Jurij Sodja, C.A.M. Socci, R. De Breuker, Christos Kassapoglou, D. Rajpal, Francesco Mitrotta

Publikováno v: Composite Structures, 275

The aim of the paper is to experimentally validate a numerical design methodology for optimizing composite wings subject to gust and fatigue loading requirements and to assess the effect of fatigue on the aeroelastic performance of the wing. Traditio

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d39af281275e3837bcece77d07174a15
https://doi.org/10.1016/j.compstruct.2021.114373

Multi-Fidelity Design of an Aeroelastically Tailored Composite Wing for Dynamic Wind-Tunnel Testing

Autor: D. Rajpal, Francesco Mitrotta, Jurij Sodja, R. De Breuker

Publikováno v: AIAA Scitech 2020 Forum: 6-10 January 2020, Orlando, FL
AIAA Scitech 2020 Forum

Aeroelastic tailoring offers an effective way to exploit the anisotropic properties of the composite materials used in lightweight aerospace structures. This paper presents a design methodology for experimental wings that employ a typical wingbox str

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::58972fa1aa3e25e9209553033bc9e9e1
https://doi.org/10.2514/6.2020-1636