Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Huitao Lyu"'
A Hinge Moment Alleviation Control Strategy for Morphing Tail Aircraft Based on a Data-Driven Method
Autor:
Rui Cao, Huitao Lyu
Publikováno v:
Actuators, Vol 13, Iss 9, p 369 (2024)
Morphing airplane technology is currently a focal point of research. For morphing airplanes, besides effective morphing strategies and control schemes, the hinge moment at the root of the vertical tail during morphing is a critical factor influencing
Externí odkaz:
https://doaj.org/article/e6efa8f3e9054219945592b8aabcae8f
Publikováno v:
Applied Sciences, Vol 13, Iss 22, p 12225 (2023)
This paper proposes a soft switching mode for electric vertical takeoff and landing (eVTOL) compound-wing unmanned aerial vehicles (UAVs) to achieve a smooth transition between modes. The proposed mode pre-compensates the lift loss with the rotary wi
Externí odkaz:
https://doaj.org/article/c4f13b5d1ae6466ca52035e2358531dc
Publikováno v:
Applied Sciences, Vol 13, Iss 11, p 6598 (2023)
Large-slenderness-ratio (LSR) aircraft exhibit more severe lateral–directional coupling compared with other aircraft, which poses a significant challenge to their flight safety, especially during high-speed maneuvers. Reliable attitude decoupling c
Externí odkaz:
https://doaj.org/article/458d8ace4e1f4538812ffb7a0297381d
Publikováno v:
Applied Sciences, Vol 13, Iss 6, p 3518 (2023)
The task of achieving a safe and short landing for a flying-wing unmanned aircraft with a three-bearing-swivel thrust vector is highly challenging. The process is further complicated due to the need to switch between multiple control modes, while als
Externí odkaz:
https://doaj.org/article/73af7d0436934667960bc06b580c4186
Publikováno v:
International Journal of Aerospace Engineering, Vol 2022 (2022)
Large-slenderness-ratio aircraft in which a large portion of the aircraft’s mass is concentrated along its centreline face the problem of severe lateral-directional coupling. Previous research has not fully considered the inertia product when condu
Externí odkaz:
https://doaj.org/article/3a7741c79b314724ab1a149cf8dfb62d
Publikováno v:
Applied Sciences; Volume 13; Issue 11; Pages: 6598
Large-slenderness-ratio (LSR) aircraft exhibit more severe lateral–directional coupling compared with other aircraft, which poses a significant challenge to their flight safety, especially during high-speed maneuvers. Reliable attitude decoupling c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=multidiscipl::6de8c9e73c752b0f4c21bc18fede8ada
Publikováno v:
Journal of Cleaner Production. 414:137525
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::214ae5ad08de49f27a444752dd9bd655
https://doi.org/10.1016/j.jclepro.2023.137525
https://doi.org/10.1016/j.jclepro.2023.137525