All Outputs (6)

Active stall flutter suppression for a revised Leishman-Beddoes Model (2023)
Journal Article
Zheng, J., Pontillo, A., Chen, L., & Whidborne, J. F. (2023). Active stall flutter suppression for a revised Leishman-Beddoes Model. Journal of Aerospace Engineering, 37(1), https://doi.org/10.1061/JAEEEZ.ASENG-5003

This paper proposes a nonlinear disturbance observer (NDO)-based sliding mode control (SMC) method to the problem of stall flutter suppression for a revised Leishman-Beddoes (L-B) model. To capture accurate aerodynamic characteristics whilst reducing... Read More about Active stall flutter suppression for a revised Leishman-Beddoes Model.

Ground vibration testing of a flexible wing: A benchmark and case study (2022)
Journal Article
Dessena, G., Ignatyev, D. I., Whidborne, J. F., Pontillo, A., & Zanotti Fragonara, L. (2022). Ground vibration testing of a flexible wing: A benchmark and case study. Aerospace, 9(8), Article 438. https://doi.org/10.3390/aerospace9080438

Beam-like flexible structures are of interest in many fields of engineering, particularly aeronautics, where wings are frequently modelled and represented as such. Experimental modal analysis is commonly used to characterise the wing’s dynamical resp... Read More about Ground vibration testing of a flexible wing: A benchmark and case study.

Aeroelastic damping estimation for a flexible high-aspect-ratio wing (2021)
Journal Article
Tsatsas, I., Pontillo, A., & Lone, M. (2022). Aeroelastic damping estimation for a flexible high-aspect-ratio wing. Journal of Aerospace Engineering, 35(2), https://doi.org/10.1061/%28ASCE%29AS.1943-5525.0001390

Estimation of aeroelastic damping for a very flexible high-aspect-ratio wing using wind-tunnel test data is presented in this work through the comparison of four different methods: half-power, half-quadratic gain, an adapted version of random decreme... Read More about Aeroelastic damping estimation for a flexible high-aspect-ratio wing.

A benchtop flight control demonstrator (2019)
Journal Article
Duran, J. R., Whidborne, J. F., Carrizales, M., & Pontillo, A. (2021). A benchtop flight control demonstrator. International Journal of Mechanical Engineering Education, 49(1), 80--97. https://doi.org/10.1177/0306419019852688

A feedback control demonstrator is described. The demonstrator is intended for the demonstration of control principles applied to flight control of fixed-wing aircraft and hence is suitable for aeronautical programmes. The demonstrator consists of a... Read More about A benchtop flight control demonstrator.

Investigating pitching moment stall through dynamic wind tunnel test (2019)
Journal Article
Pontillo, A., Yusuf, S., Lopez, G., Rennie, D., & Lone, M. (2020). Investigating pitching moment stall through dynamic wind tunnel test. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 234(2), 267-279. https://doi.org/10.1177/0954410019861853

Experimental characterisation of aircraft dynamic stall can be a challenging and complex system identification activity. In this article, the authors present a method that combines dynamic wind tunnel testing with parameter estimation techniques to s... Read More about Investigating pitching moment stall through dynamic wind tunnel test.

Parameters estimation methodology for the nonlinear rolling motion of finned cylindrical body (2018)
Journal Article
Abadir, M., Yusuf, S., Pontillo, A., & Lone, M. (2019). Parameters estimation methodology for the nonlinear rolling motion of finned cylindrical body. Aerospace Science and Technology, 84, 782-798

Identification of nonlinear roll dynamics of finned cylindrical bodies is a critical step when assessing free motion stability and trajectories of aerially dispensed munitions or decoys. In this paper the authors present a parameter estimation proces... Read More about Parameters estimation methodology for the nonlinear rolling motion of finned cylindrical body.