D4.1 - Advanced UAV Design ...
This report presents the collaborative work done between CO.RI.S.T.A. and HYPERION SEVEN to come up with a design for the drone that will be used for the FlyRadar project. This report concludes first that the optimal design t o be used is a classical quadcopter, and one suitable for the anticipated...
Main Authors: | , , , |
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Format: | Text |
Language: | unknown |
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Zenodo
2021
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Subjects: | |
Online Access: | https://dx.doi.org/10.5281/zenodo.7764214 https://zenodo.org/record/7764214 |
Summary: | This report presents the collaborative work done between CO.RI.S.T.A. and HYPERION SEVEN to come up with a design for the drone that will be used for the FlyRadar project. This report concludes first that the optimal design t o be used is a classical quadcopter, and one suitable for the anticipated payload weight would be the TUNDRA, built by HEXADRONE. Various mechanical pieces will have to be built in order to mount the radar and its various antennas onto the drone. Finally, it was first foreseen that the use of a tether between the drone and a ground station could be utilized in order to power the drone indefinitely and have a fiber optic line to the ground, which would allow to re- trieve the captured data in real time and avoid to need of an on-board computer. However, the radar design of CO.RI.S.T.A. includes a computer small enough that an optical link is no longer needed. Moreover, in the aim of having t he drone fly in the desert (terrestrial terrains analogous to Mars), it is probably better to ... |
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