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Armanini, S.F. (author), Caetano, J. V. (author), de Visser, C.C. (author), Pavel, M.D. (author), de Croon, G.C.H.E. (author), Mulder, M. (author)
Despite significant interest in tailless flapping-wing micro aerial vehicle designs, tailed configurations are often favoured, as they offer many benefits, such as static stability and a simpler control strategy, separating wing and tail control. However, the tail aerodynamics are highly complex due to the interaction between the unsteady...
journal article 2019
document
Quaranta, Giuseppe (author), Pavel, M.D. (author), Barakos, George (author), White, Mark (author), Mulder, M. (author)
Helicopters are currently used in important applications providing a valuable contribution to society and economic growth. Thanks to their operational flexibility it is possible to accomplish increasingly complex missions. If the expansion of the usage of rotorcraft is to follow the pace of growth achieved by the fixed-wing public transport...
journal article 2018
document
Miletovic, I. (author), Pavel, M.D. (author), Stroosma, O. (author), Pool, D.M. (author), van Paassen, M.M. (author), Wentink, Mark (author), Mulder, M. (author)
Eigenmode distortion (EMD) is a novel methodology developed to study the degradation of perceived vehicle dynamics as a result of motion cueing algorithms (MCA’s) applied in rotorcraft 2ight simulators. This paper brie2y introduces EMD and subsequently describes its application in a pilot-in-the-loop experiment conducted on the SIMONA Research...
conference paper 2018
document
Scaramuzzino, P.F. (author), D’Intino, Giulia (author), Geluardi, Stefano (author), Pavel, M.D. (author), Pool, D.M. (author), Stroosma, O. (author), Mulder, M. (author), Bülthoff, Heinrich H. (author)
Today, simulators are achieving levels of complexity and cost that are comparable to those of the aircraft they should replace. For this reason, questions have been raised, in both the technical and training communities, on the required level of simulation 1delity for effective pilot training. Computer Based Trainers (CBTs) are not currently...
conference paper 2018
document
Miletovic, I. (author), Pool, D.M. (author), Stroosma, O. (author), Pavel, M.D. (author), Wentink, M (author), Mulder, M. (author)
The fidelity of a rotorcraft flight simulator is influenced by many factors, such as the vehicle dynamic model and the motion cueing algorithm (MCA). To quantify the fidelity of a simulator objectively requires detailed knowledge of human pilot perception and control behaviour that is not yet available. As a consequence, subjective...
conference paper 2017
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