LUTHFIE TSAQIF, LAUDZA (2024) RANCANG BANGUN BATANG VTOL PADA UAV SKY-BEEJO SEBAGAI TEMPAT PENEMPATAN PROPULSI UAV VERTICAL TAKE OFF LANDING. Skripsi thesis, Institut Teknologi Dirgantara Adisutjipto.
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Abstract
In research with the theme of adding VTOL rods, of course a lot of changes or overhauls are needed in the load, structure, materials used, propulsion and also the design of the UAV itself. Therefore, significant changes will also be made to the VTOL rod itself so that it can be adequate so that a UAV can take off and land. The addition of VTOL rods to the UAV wing structure, which was previously a Fixed Wing type UAV then changed to a UAV that can perform VTOL or Vertical Take off Landing. Using the Margin Of Safety method. From this research, the results obtained obtained ARM VTOL configuration with a length of 85cm using aluminum and placed at a distance of 50cm from the fuselage. From the simulation get a margin of safety value of 5.1339.
Item Type: | Thesis (Skripsi) |
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Subjects: | T Technology > T Technology (General) |
Divisions: | Institut Teknologi Dirgantara Adisujtipto > Teknik Dirgantara |
Depositing User: | Mr Luthfie laudzatsaqif |
Date Deposited: | 06 May 2024 02:43 |
Last Modified: | 06 May 2024 02:43 |
URI: | http://eprints.stta.ac.id/id/eprint/1694 |
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