Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Thomas R. Shearwood"'
Publikováno v:
IEEE Access, Vol 11, Pp 61401-61411 (2023)
Attitude control of tailless aircraft is typically achieved through a system of trailing-edge flaps that produce coupled control effects in pitch, roll and yaw due to changes in lift and drag distributions. This paper presents a novel control allocat
Externí odkaz:
https://doaj.org/article/2d2b186019fc421db6d52b6602e7d384
Publikováno v:
Aerospace, Vol 7, Iss 10, p 150 (2020)
Tailless aircraft without vertical stabilisers typically use drag effectors in the form of spoilers or split flaps to generate control moments in yaw. This paper introduces a novel control allocation method by which full three-axis control authority
Externí odkaz:
https://doaj.org/article/0a7002ff30b54726810c8aff3fcea255
Autor:
Bill Crowther, Mostafa Nabawy, Roland Penty Geraets, Mark K. Quinn, Sam Weigert, Clyde Warsop, Matt Forster, Lucia Axani, Thomas R. Shearwood
Publikováno v:
AIAA SCITECH 2023 Forum.
Autor:
Bill Crowther, Thomas R. Shearwood, Mostafa Nabawy, Roland Penty Geraets, Mark K. Quinn, Sam Weigert, Clyde Warsop, Matt Forster, Lucia Axani
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
AIAA AVIATION 2021 FORUM.
Publikováno v:
AIAA Scitech 2021 Forum.
Publikováno v:
Aerospace, Vol 7, Iss 150, p 150 (2020)
Aerospace
Volume 7
Issue 10
Aerospace
Volume 7
Issue 10
Tailless aircraft without vertical stabilisers typically use drag effectors in the form of spoilers or split flaps to generate control moments in yaw. This paper introduces a novel control allocation method by which full three-axis control authority
Publikováno v:
AIAA AVIATION 2020 FORUM.
Publikováno v:
AIAA Aviation 2019 Forum.