TY - GEN
T1 - Unmanned aerial vehicle design for pressure washing building facades in Lima Metropolitan Area using hydrogen fuel cell
AU - Melgarejo, Joaquin
AU - Furukawa, Roberto
N1 - Publisher Copyright:
© 2022 IEEE.
PY - 2022
Y1 - 2022
N2 - The following paper has the purpose of presenting an innovative solution for building facade cleaning using an unmanned aerial vehicle (UAV) that employs pressure washing technique and hydrogen fuel cell (HFC) technology to enhance flight autonomy. Indeed, the main design stages are both stated and explained within the paper. However, the design is separated in two stages: Conceptual and Preliminary. Thus, it begins with the research statement, state of the art revision and conceptual design proposal. Then, it continues with the development of the propulsion system, which uses a proposed recursive methodology for estimating, selecting, and then confirming all the inter-dependent elements such as motors, propellers, fuel cell and hydrogen amount. As the drone is treated as a mechatronic machine, the following design explores certain domains that help build it, such as: Mechanical, Electrical and Control. The Mechanical domain emphasizes on frame design, material selection, resistance calculations, pressure washing gun recoil analysis, and finite element and aerodynamic simulations. The Electrical domain focuses on component selection and power consumption verification while the last domain proposes flow diagrams and a PID control diagram based on an hexacopter mathematical modelling. Finally, the main flight parameters are simulated on SIMULINK, obtaining appropriate stabilizing and response times according to limitations cited.
AB - The following paper has the purpose of presenting an innovative solution for building facade cleaning using an unmanned aerial vehicle (UAV) that employs pressure washing technique and hydrogen fuel cell (HFC) technology to enhance flight autonomy. Indeed, the main design stages are both stated and explained within the paper. However, the design is separated in two stages: Conceptual and Preliminary. Thus, it begins with the research statement, state of the art revision and conceptual design proposal. Then, it continues with the development of the propulsion system, which uses a proposed recursive methodology for estimating, selecting, and then confirming all the inter-dependent elements such as motors, propellers, fuel cell and hydrogen amount. As the drone is treated as a mechatronic machine, the following design explores certain domains that help build it, such as: Mechanical, Electrical and Control. The Mechanical domain emphasizes on frame design, material selection, resistance calculations, pressure washing gun recoil analysis, and finite element and aerodynamic simulations. The Electrical domain focuses on component selection and power consumption verification while the last domain proposes flow diagrams and a PID control diagram based on an hexacopter mathematical modelling. Finally, the main flight parameters are simulated on SIMULINK, obtaining appropriate stabilizing and response times according to limitations cited.
KW - frame design
KW - HFC
KW - pressure washing
KW - SIMULINK
KW - UAV
UR - http://www.scopus.com/inward/record.url?scp=85138828613&partnerID=8YFLogxK
U2 - 10.1109/INTERCON55795.2022.9870088
DO - 10.1109/INTERCON55795.2022.9870088
M3 - Conference contribution
AN - SCOPUS:85138828613
T3 - Proceedings of the 2022 IEEE 29th International Conference on Electronics, Electrical Engineering and Computing, INTERCON 2022
BT - Proceedings of the 2022 IEEE 29th International Conference on Electronics, Electrical Engineering and Computing, INTERCON 2022
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 29th IEEE International Conference on Electronics, Electrical Engineering and Computing, INTERCON 2022
Y2 - 11 August 2022 through 13 August 2022
ER -