TY - GEN
T1 - Cargo transportation strategy using T3-multirotor UAV
AU - Lee, Seung Jae
AU - Lee, Dongjae
AU - Kim, H. Jin
N1 - Publisher Copyright:
© 2019 IEEE.
PY - 2019/5
Y1 - 2019/5
N2 - In this paper, we introduce a cargo transportation method with a new type of multi-rotor UAV platform known as T3-multirotor, to achieve stable and constant flight performance regardless of the type of cargo attached to the fuselage. The T3-multirotor, which consists of the 'Thrust Generating Part' and the 'Fuselage Part', can directly control the relative attitude between the two parts using the novel servomechanism. By utilizing the servomechanism with the proposed relative attitude control strategy, the T3-multirotor with cargo attached to the fuselage part can behave as a multi-rotor with only the moment of inertia of the thrust generating part during entire transportation. This allows the T3-multirotor to achieve the reliable performance in the event of any cargo being attached to the fuselage, achieving stable platform motion control. Detailed hardware description and dynamic analysis of T3-Multirotor is performed in this paper, and the validity of the proposed control strategy is also analyzed. The feasibility of the proposed control strategy is verified through experimental results with analysis.
AB - In this paper, we introduce a cargo transportation method with a new type of multi-rotor UAV platform known as T3-multirotor, to achieve stable and constant flight performance regardless of the type of cargo attached to the fuselage. The T3-multirotor, which consists of the 'Thrust Generating Part' and the 'Fuselage Part', can directly control the relative attitude between the two parts using the novel servomechanism. By utilizing the servomechanism with the proposed relative attitude control strategy, the T3-multirotor with cargo attached to the fuselage part can behave as a multi-rotor with only the moment of inertia of the thrust generating part during entire transportation. This allows the T3-multirotor to achieve the reliable performance in the event of any cargo being attached to the fuselage, achieving stable platform motion control. Detailed hardware description and dynamic analysis of T3-Multirotor is performed in this paper, and the validity of the proposed control strategy is also analyzed. The feasibility of the proposed control strategy is verified through experimental results with analysis.
UR - http://www.scopus.com/inward/record.url?scp=85071507992&partnerID=8YFLogxK
U2 - 10.1109/ICRA.2019.8794203
DO - 10.1109/ICRA.2019.8794203
M3 - Conference contribution
AN - SCOPUS:85071507992
T3 - Proceedings - IEEE International Conference on Robotics and Automation
SP - 4168
EP - 4173
BT - 2019 International Conference on Robotics and Automation, ICRA 2019
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2019 International Conference on Robotics and Automation, ICRA 2019
Y2 - 20 May 2019 through 24 May 2019
ER -