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Fabrication of solar energy UAV
Published in International Journal of Ambient Energy, 2020
M. Saleem, E. Gopi, R. Ramesh Kumar
These UAVs could be carried in a briefcase, backpack, or the storage area of a personal vehicle. The ideal UAV would also deploy with little effort and remain deployed reliably during flight. Many larger folding wing aircrafts have relied on a complicated system of pin joints, swivels, hinges, cables, and locks in order to provide sufficient range of motion and stability for the folding wings (How, King, and Kuwata, 2004). Other applications like foldable fins for tube-launched missiles often rely on similarly complicated systems. With limited weight and space for UAVs, conventional rigid-body folding mechanisms have been even more difficult to achieve. In such cases, compliant mechanisms offer many potential advantage. Compliant mechanisms can be used to facilitate additional space and cost savings due to a potential reduction in part count and increased function-sharing among parts.