Výsledky vyhledávání - "Stroosma, O."

Akademický článek

Incremental Nonlinear Dynamic Inversion Control for Hydraulic Hexapod Flight Simulator Motion Systems

Autor: Huang, Yingzhi ^*, Pool, D.M. ^*, Stroosma, O. ^*, Chu, Q.P. ^*

Publikováno v: In IFAC PapersOnLine July 2017 50(1):4294-4299

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Akademický článek

Improved Stewart platform state estimation using inertial and actuator position measurements

Autor: Miletović, I., Pool, D.M., Stroosma, O., van Paassen, M.M., Chu, Q.P.

Publikováno v: In Control Engineering Practice May 2017 62:102-115

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Akademický článek

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Akademický článek

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Rotorcraft Flight Simulation Model Fidelity Improvement and Assessment

Autor: Greiser, Steffen, Pavel, M.D., Stroosma, O., Yavrucuk, Ilkay, White, Mark D., Padfield, Gareth D, Cameron, Neil, Prasad, J.V.R., Guner, Feyyaz

Rotorcraft flight dynamics simulation models require high levels of fidelity to be suitable as prime items in support of life cycle practices, particularly vehicle and control design and development, and system and trainer certification. On the civil

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=narcis______::8001595117fdf6da670ea7f04cd02034
http://resolver.tudelft.nl/uuid:2800f932-9824-4d07-83eb-9574dbb81c92

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Effectiveness of a Computer-Based Helicopter Trainer for Initial Hover Training

Autor: Scaramuzzino, Paolo Francesco, D’Intino, Giulia, Geluardi, Stefano, Pavel, M.D., Pool, D.M., Stroosma, O., Mulder, Max, Bülthoff, Heinrich H., Hermans, C.

Publikováno v: Proceedings of the 44th European Rotorcraft Forum: Delft, The Netherlands, 2018
Proceedings of the 44th European Rotorcraft Forum

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 simu

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=narcis______::aaa2ac4659edc4448674413dc570aa8e
http://resolver.tudelft.nl/uuid:d929d485-959a-4733-8d9b-a8da26bb42c9

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Eigenmode Distortion as a Novel Criterion for Motion Cueing Fidelity in Rotorcraft Flight Simulation

Autor: Miletović, I., Pavel, M.D., Stroosma, O., Pool, D.M., van Paassen, M.M., Wentink, Mark, Mulder, Max, Hermans, C.

Publikováno v: Proceedings of the 44th European Rotorcraft Forum: Delft, The Netherlands, 2018
Proceedings of the 44th European Rotorcraft Forum

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 subseque

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=narcis______::4d4f2ccc60389599438626d2695aa3e2
http://resolver.tudelft.nl/uuid:19fcd84a-a31f-4302-a92e-c26bed99101f

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Prediction and simulator verification of state-space rotor modelling on helicopter manoeuvring flight

Autor: Gori, R., Massimo Gennaretti, Pavel, M. D., Stroosma, O., Miletović, I.

Publikováno v: Proceedings of the 41st European Rotorcraft Rorum 2015, Munich (Germany), Sept. 1-4, 2015
Scopus-Elsevier

Among the many fundamental components of a flight simulator, the mathematical representation of the vehicle dynamics stands out for complexity and importance. This is especially true for helicopters, for which the complex dynamics involved prevents s

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::dbc0768d6ae8a155aaf1914c403ee1eb
http://resolver.tudelft.nl/uuid:fc7ec49c-aa47-416c-a594-525193707667

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Incremental Nonlinear Dynamic Inversion Control for Hydraulic Hexapod Flight Simulator Motion Systems

Autor: Huang, Y., Pool, D.M., Stroosma, O., Chu, Q. P., Dochain, D., Henrion, D., Peaucelle, D.

Publikováno v: IFAC-PapersOnLine, 50

Hydraulic driven manipulators face serious control problems due to the nonlinear system dynamics and model and parametric uncertainties of hydraulic actuators. In this paper, a novel sensor-based Incremental Nonlinear Dynamic Inversion controller is

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=narcis______::28557c04b626b8c795ce7511409e9578
http://resolver.tudelft.nl/uuid:90a959c1-c1a2-49b0-b04c-3c4d8585ce5d

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Extending the Objective Motion Cueing Test to Measure Rotorcraft Simulator Motion Characteristics

Autor: Dalmeijer, W., Miletović, I., Stroosma, O., Pavel, M.D.

Publikováno v: 73rd Annual AHS International Forum and Technology Display: The Future of Vertical Flight 2017 (AHS Forum 73)
73rd Annual AHS International Forum and Technology Display

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