Zobrazeno 1 - 10
of 346
pro vyhledávání: '"phugoid"'
Autor:
Castaldi, Paolo1 paolo.castaldi@unibo.it, Mimmo, Nicola1 nicola.mimmo2@unibo.it, Simani, Silvio2 silvio.simani@unife.it
Publikováno v:
Sensors (14248220). Oct2017, Vol. 17 Issue 10, p2202. 19p.
Publikováno v:
Aviation, Vol 25, Iss 1, Pp 22-34 (2021)
This paper discusses the development of a ground based variable stability flight simulator. The simulator is designed to meet the pilot training requirements on flying qualities. Such a requirement arose from a premier Flight-Testing School of the In
Externí odkaz:
https://doaj.org/article/e7f0b7471bcd41ff8eb990123b25c1ae
Publikováno v:
Journal of Mechatronics, Electrical Power, and Vehicular Technology, Vol 11, Iss 2, Pp 86-94 (2020)
The longitudinal altitude holding control system (LAHCS) of wing in surface effect (WiSE) vehicle has been developed using Simulink/Matlab. The LAHCS is designed to maintain the altitude of the vehicle stands at 1 m above the surface, with a maximum
Externí odkaz:
https://doaj.org/article/515cf044683749c3828248c101d6c10e
Autor:
Srinathkumar, S.1
Publikováno v:
Journal of the American Helicopter Society. Jan2019, Vol. 64 Issue 1, p1-12. 12p.
Autor:
Giota, Argyro, Roszkowska, Aleksandra
This report focuses on the utilisation of flight mechanics in the context of aircraftconceptual design to assess stability, control, and motion characteristics. The pri-mary objective is to acquire the equations of motion and implement longitudinalst
Externí odkaz:
http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-196520
Publikováno v:
ISA Transactions; Dec2018, Vol. 83, p176-188, 13p
Autor:
Kohler, Austin J.
Publikováno v:
All Graduate Theses and Dissertations
The United States Air Force (USAF) will likely seek to remove the vertical tail of next-generation fighter aircraft. This work seeks to characterize the static and dynamic stability and handling qualities of a vertical-tailless aircraft concept that
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::84613f9e1d53810c31295dadc9106f5e
https://digitalcommons.usu.edu/etd/8675
https://digitalcommons.usu.edu/etd/8675
Publikováno v:
Journal of Mechatronics, Electrical Power, and Vehicular Technology, Vol 11, Iss 2, Pp 86-94 (2020)
The longitudinal altitude holding control system (LAHCS) of wing in surface effect (WiSE) vehicle has been developed using Simulink/Matlab. The LAHCS is designed to maintain the altitude of the vehicle stands at 1 m above the surface, with a maximum
Autor:
DZERKELIS, V., LUKOŠEVIČIUS, V., GIRKONTAS, E., KERŠYS, R., SAR, H., MAKARAS, R., SKVIRECKAS, R.
Publikováno v:
Mechanika; 2018, Vol. 24 Issue 1, p65-73, 9p, 4 Diagrams, 3 Charts, 5 Graphs
Autor:
Chatterjee, Sankar, Templin, R. Jack
Publikováno v:
Proceedings of the National Academy of Sciences of the United States of America, 2007 Jan . 104(5), 1576-1580.
Externí odkaz:
https://www.jstor.org/stable/25426331