TY - GEN
T1 - Mechatronic Design of an Omnidirectional Octorotor UAV
AU - Hamandi, Mahmoud
AU - Ali, Abdullah Mohamed
AU - Evangeliou, Nikolaos
AU - Chaikalis, Dimitris
AU - Tzes, Anthony
AU - Kyriakopoulos, Konstantinos
AU - Khorrami, Farshad
N1 - Publisher Copyright:
© 2024 IEEE.
PY - 2024
Y1 - 2024
N2 - The design of an omnidirectional octorotor (OmniOcta) is the scope of this article. The pose of the UAV's thrusters is computed via an optimization algorithm that guarantees the omnidirectionality of the platform. The thrusters' positions are restricted in a semispherical volume with different polar coordinates while their pose is determined in order to avoid the interaction between their propellers' air-funnels. The octorotor is manufactured using 3D printed parts and its employed electronics were selected so as to have the smallest weight. The number of thrusters was then selected as the minimal number that could lift the platform's weight in all rotation directions with the chosen electronic and aerodynamic components. Simulations were conducted to show the capacity of the UAV to lift its weight, while experiments were conducted to identify the allocation matrix of the constructed UAV.
AB - The design of an omnidirectional octorotor (OmniOcta) is the scope of this article. The pose of the UAV's thrusters is computed via an optimization algorithm that guarantees the omnidirectionality of the platform. The thrusters' positions are restricted in a semispherical volume with different polar coordinates while their pose is determined in order to avoid the interaction between their propellers' air-funnels. The octorotor is manufactured using 3D printed parts and its employed electronics were selected so as to have the smallest weight. The number of thrusters was then selected as the minimal number that could lift the platform's weight in all rotation directions with the chosen electronic and aerodynamic components. Simulations were conducted to show the capacity of the UAV to lift its weight, while experiments were conducted to identify the allocation matrix of the constructed UAV.
KW - Omnidirectional UAS
KW - UAV Design
UR - http://www.scopus.com/inward/record.url?scp=85197343069&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85197343069&partnerID=8YFLogxK
U2 - 10.1109/ICARA60736.2024.10553043
DO - 10.1109/ICARA60736.2024.10553043
M3 - Conference contribution
AN - SCOPUS:85197343069
T3 - 2024 10th International Conference on Automation, Robotics, and Applications, ICARA 2024
SP - 300
EP - 304
BT - 2024 10th International Conference on Automation, Robotics, and Applications, ICARA 2024
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 10th International Conference on Automation, Robotics, and Applications, ICARA 2024
Y2 - 22 February 2024 through 24 February 2024
ER -