A Novel Force Measurement Design for the Actuator of a Quadrotor Unmanned Aerial Vehicle
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Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-97-5504-2_82
Reference10 articles.
1. Gün, A.: Attitude control of a quadrotor using PID controller based on differential evolution algorithm. Expert Syst. Appl. 229, 120518 (2023). https://doi.org/10.1016/j.eswa.2023.120518
2. Gandolfo, D.C., Rosales, C.D., Salinas, L.R., Gimenez, J., Carelli, R.: Low-cost position and force measurement system for payload transport using UAVs. Int. J. Autom. Comput. 18(4), 594–604 (2021). https://doi.org/10.1007/s11633-021-1281-4
3. Ahmad, F., Kumar, P., Dobriyal, R., Patil, P.P.: Estimation of the thrust coefficient of a quadcopter propeller using computational fluid dynamics. IOP Conf. Ser. Mater. Sci. Eng. 1116(1), 012095 (2021). https://doi.org/10.1088/1757-899X/1116/1/012095
4. Szőke, Z., Novotňák, J., Lipovský, P., Šmelko, M., Filko, M., Košuda, M.: Design of workplace for multirotor UAV parameters measurement. In: 2020 New Trends in Aviation Development (NTAD), pp. 236–239 (2020). https://doi.org/10.1109/NTAD51447.2020.9379110
5. Cruzatty, C., Sarmiento, E., Valencia, E., Cando, E.: Design methodology of a UAV propeller implemented in monitoring activities. Mater. Today Proc. 49, 115–121 (2022). https://doi.org/10.1016/j.matpr.2021.07.481
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