Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Quoc Viet Luong"'
Publikováno v:
Actuators, Vol 12, Iss 4, p 160 (2023)
In recent years, there has been an increase in the development of medical robots to enhance interventional MRI-guided therapies and operations. Magnetic resonance imaging (MRI) surgical robots are particularly attractive due to their ability to provi
Externí odkaz:
https://doaj.org/article/9f7a236021974cb5ba6b8b99b368ee7c
Publikováno v:
Applied Sciences, Vol 11, Iss 8, p 3667 (2021)
Due to their extensive use in various applications, helicopters need to be able to land in a variety of conditions. Typically, a helicopter landing gear system with skids or passive wheel-dampers is designed based on only one critical touchdown condi
Externí odkaz:
https://doaj.org/article/3a15d1d04afe4c13bd82ee9ed42812cc
Publikováno v:
Applied Sciences, Vol 10, Iss 17, p 5962 (2020)
A typical oleo-pneumatic shock-absorbing strut (classic traditional passive damper) in aircraft landing gear has a metering pin extending through the orifice, which can vary the orifice area with the compression and extension of the damper strut. Bec
Externí odkaz:
https://doaj.org/article/0c6b8c8ff68c4ecdad41a7fb8a537470
Publikováno v:
Applied Sciences, Vol 10, Iss 4, p 1459 (2020)
A landing gear of an aircraft is required to function at touchdown in different landing scenarios with parametric uncertainties. A typical passive damper in a landing gear has limited performance in differing landing scenarios, which can be overcome
Externí odkaz:
https://doaj.org/article/67a29688c25c48f489d594a1c787e9cd
Publikováno v:
Journal of the Korean Society for Precision Engineering. 39:669-674
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f7bf3f89262fc8ab44fa4823fa5af7d5
https://doi.org/10.7736/jkspe.022.067
https://doi.org/10.7736/jkspe.022.067
Publikováno v:
Applied Sciences
Volume 10
Issue 4
Applied Sciences, Vol 10, Iss 4, p 1459 (2020)
Volume 10
Issue 4
Applied Sciences, Vol 10, Iss 4, p 1459 (2020)
A landing gear of an aircraft is required to function at touchdown in different landing scenarios with parametric uncertainties. A typical passive damper in a landing gear has limited performance in differing landing scenarios, which can be overcome
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2bbc8c7879313c4f8e633614187d8ee2
Publikováno v:
Applied Sciences, Vol 12, Iss 400, p 400 (2022)
Applied Sciences; Volume 12; Issue 1; Pages: 400
Applied Sciences; Volume 12; Issue 1; Pages: 400
This paper adopts an intelligent controller based on supervised neural network control for a magnetorheological (MR) damper in an aircraft landing gear. An MR damper is a device capable of adjusting the damping force by changing the magnetic field ge
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2e6641373706e7f062860a9a9c07db9f
https://doi.org/10.3390/app12010400
https://doi.org/10.3390/app12010400
Publikováno v:
Applied Sciences, Vol 11, Iss 3667, p 3667 (2021)
Applied Sciences
Volume 11
Issue 8
Applied Sciences
Volume 11
Issue 8
Due to their extensive use in various applications, helicopters need to be able to land in a variety of conditions. Typically, a helicopter landing gear system with skids or passive wheel-dampers is designed based on only one critical touchdown condi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cc19af01ac79471bb9bbccbb24299e6c
https://doi.org/10.3390/app11083667
https://doi.org/10.3390/app11083667
Publikováno v:
Applied Sciences, Vol 10, Iss 5962, p 5962 (2020)
Applied Sciences
Volume 10
Issue 17
Applied Sciences
Volume 10
Issue 17
A typical oleo-pneumatic shock-absorbing strut (classic traditional passive damper) in aircraft landing gear has a metering pin extending through the orifice, which can vary the orifice area with the compression and extension of the damper strut. Bec
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8f17e753785779d9a584eca7e103b9f0
https://doi.org/10.3390/app10175962
https://doi.org/10.3390/app10175962
Publikováno v:
Aerospace, Vol 10, Iss 11, p 951 (2023)
Aircraft landing gear equipped with a magnetorheological (MR) damper is a semi-active system that contains nonlinear behavior, disturbances, uncertainties, and delay times that can have a huge impact on the landing’s performance. To solve this prob
Externí odkaz:
https://doaj.org/article/36541a2328f1404c88076fb34f23d9da