Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Ashim Panta"'
Publikováno v:
Drones, Vol 7, Iss 8, p 494 (2023)
This study investigates the use of rapidly actuated leading-edge and trailing-edge control surfaces to improve the control authority of small fixed-wing drones. Static and dynamic characteristics were investigated and presented in two separate papers
Externí odkaz:
https://doaj.org/article/e37be48b4add433f90c87def8809a30c
Publikováno v:
Journal of Aerospace Technology and Management, Vol 10 (2018)
Parachute Systems (PS) can be readily used by small Unmanned Aircraft Systems (UAS) for risk mitigation and aircraft recovery. To date there has been limited research into the fundamental dynamics of parachutes at low Reynolds numbers,with existing s
Externí odkaz:
https://doaj.org/article/b707ce1bd2c04fe49cb226c5ead9cf8b
Publikováno v:
Progress in Aerospace Sciences. 102:122-135
© 2018 Elsevier Ltd Micro Air Vehicles (MAVs) have the potential to revolutionize our capabilities in gathering information, monitoring situations, and surveillance. They are required to maneuver in and around obstacles as well as negotiate atmosphe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4d9951d5b12e94042d57ddceecf4de6f
https://doi.org/10.1016/j.paerosci.2018.07.005
https://doi.org/10.1016/j.paerosci.2018.07.005
Publikováno v:
International Journal of Micro Air Vehicles. 10:254-261
The stability of small unmanned air systems can be challenged by turbulence during low-altitude flight in cluttered urban environments. This paper explores the benefits of a tandem wing aircraft configuration with the implementation of a pressure-bas
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::07e100dc2792228364526fb8373362a9
https://doi.org/10.1177/1756829318794167
https://doi.org/10.1177/1756829318794167
Publikováno v:
ANZCC
For a fixed-wing unmanned aerial vehicle flight in turbulent environments, distributing aerodynamic load of single aileron through multiple segments can provide rapid actuation, precise roll and heave control while also having the potential to improv
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f1dceafdbc08ca7f103f128dca07da0e
https://doi.org/10.1109/anzcc47194.2019.8945775
https://doi.org/10.1109/anzcc47194.2019.8945775
Publikováno v:
AIAA Scitech 2019 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::48002d49fe5c1902f92405895a6102af
https://doi.org/10.2514/6.2019-1397
https://doi.org/10.2514/6.2019-1397
Publikováno v:
Aerospace Science and Technology. 99:105563
The use of a leading-edge hinged control surface, as opposed to a traditional trailing-edge hinged control surface, is investigated in the context of improving control authority of fixed-wing Micro Air Vehicles when subject to gusts. Static and dynam
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::269d9c608693b32af1e8a62816df51a7
https://doi.org/10.1016/j.ast.2019.105563
https://doi.org/10.1016/j.ast.2019.105563
Publikováno v:
Journal of Aerospace Technology and Management v.10 2018
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Volume: 10, Article number: e1218, Published: 08 MAR 2018
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Volume: 10, Article number: e1218, Published: 08 MAR 2018
Parachute Systems (PS) can be readily used by small Unmanned Aircraft Systems (UAS) for risk mitigation and aircraft recovery. To date there has been limited research into the fundamental dynamics of parachutes at low Reynolds numbers, with existing
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9cd8c629ca8117fb631b347b7dc94bab
https://doi.org/10.5028/jatm.v10.752
https://doi.org/10.5028/jatm.v10.752