Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Michel Joël Tchatchueng Kammegne"'
Autor:
Lucian Teodor Grigorie, Youssef Mébarki, Michel Joël Tchatchueng Kammegne, Ruxandra Mihaela Botez, Mahmoud Mamou
Publikováno v:
Chinese Journal of Aeronautics, Vol 30, Iss 2, Pp 561-576 (2017)
In aircraft wing design, engineers aim to provide the best possible aerodynamic performance under cruise flight conditions in terms of lift-to-drag ratio. Conventional control surfaces such as flaps, ailerons, variable wing sweep and spoilers are use
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::107e358f9b3f7b816544c23124682f92
https://doi.org/10.1016/j.cja.2017.02.001
https://doi.org/10.1016/j.cja.2017.02.001
Autor:
Lucian Teodor Grigorie, Andreea Koreanschi, Ruxandra Mihaela Botez, Michel Joël Tchatchueng Kammegne
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 230:132-145
The paper presents the design and the experimental validation of a position controller for a morphing wing application. The actuation mechanism uses two DC motors to rotate two eccentric shafts which morph a flexible skin along two parallel actuation
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::edd761576d820a7ba1af55ff9b2312a8
https://doi.org/10.1177/0954410015588573
https://doi.org/10.1177/0954410015588573
Autor:
Lucian Teodor Grigorie, Yvan Tondji, Mahmoud Mamou, Ruxandra Mihaela Botez, Michel Joël Tchatchueng Kammegne, Youssef Mébarki
A morphing wing can improve the aircraft aerodynamic performance by changing the wing airfoil depending on the flight conditions. In this paper, a new control methodology is presented for a morphing wing demonstrator tested in a subsonic wind tunnel
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::487233b56acc25ccc28bcf1417e76e8a
https://nrc-publications.canada.ca/eng/view/object/?id=a2fab89e-2253-4ed4-9ebe-6dfac57ca7b3
https://nrc-publications.canada.ca/eng/view/object/?id=a2fab89e-2253-4ed4-9ebe-6dfac57ca7b3
Autor:
Michel Joël Tchatchueng Kammegne, Youssef Mébarki, Ruxandra Mihaela Botez, Lucian Teodor Grigorie, Mahmoud Mamou
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::70709d9a4406df60dbbc0daf29c3a7a1
https://doi.org/10.2514/6.2016-3390
https://doi.org/10.2514/6.2016-3390
Actuation Mechanism Control in a Morphing Application with a Full-scaled Portion of an Aircraft Wing
Publikováno v:
Modelling, Identification and Control / 834: Parallel and Distributed Computing and Networks / 835: Software Engineering.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2c6e2c93dc444dd55ea1bb601fa879ae
https://doi.org/10.2316/p.2016.830-031
https://doi.org/10.2316/p.2016.830-031
Autor:
Michel Joël Tchatchueng Kammegne, Ruxandra Mihaela Botez, Teordor L. Grigorie, Duc-Hien Nguyen
Publikováno v:
AIAA Modeling and Simulation Technologies Conference.
Aircraft wings are generally designed and optimized to give the best possible performance for cruise flight conditions. Using conventional control surfaces such as flaps, ailerons, variable wing sweep and spoilers, the structure of aircraft wings is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c40fdbc38b688f64d0691fa43c2e138d
https://doi.org/10.2514/6.2015-2499
https://doi.org/10.2514/6.2015-2499
Publikováno v:
23rd AIAA/AHS Adaptive Structures Conference.
The modeling, simulation and control of an electrical actuator used for morphing wing are presented. Because of its small size, this actuator belongs to the category of miniature actuators. Before proceeding with the modeling, the actuator was tested
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7cbec3bc954708f965c73222c890c967
https://doi.org/10.2514/6.2015-1256
https://doi.org/10.2514/6.2015-1256
Publikováno v:
Modelling, Identification and Control / 827: Computational Intelligence.
This paper describes the design of a double loop fuzzy logic position and torque controller for wing morphing using brushed DC motors as actuators. The DC motor is used in this application as an actuator to change the shape of a wing upper surface. T
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e0b08e1dbabaee7ed63857cc928df251
https://doi.org/10.2316/p.2015.826-022
https://doi.org/10.2316/p.2015.826-022
Autor:
Teodor Lucian Grigorie, Michel Joël Tchatchueng Kammegne, Andreea Koreanschi, Ruxandra Mihaela Botez
Publikováno v:
Modelling, Identification and Control.
Conventional or brushed DC motors are often used for many industrial applications. A large variety of these motors is found in automation, medical, robotics and aeronautical fields. In this paper, the design and experimental validation of a position
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bf534287b8319ff09235fdb2b9006c5a
https://doi.org/10.2316/p.2014.809-041
https://doi.org/10.2316/p.2014.809-041