VIBRATION RESPONSE ANALYSIS ON A UAV WITH A HIGH ASPECT RATIO WING TO TURBULENT LOAD AT LOW ALTITUDE (HALE ITB V4 CASE STUDY)
As a high altitude platform with a high aspect ratio, the HALE unmanned aircraft is prone to structural failure when flying at low altitudes due to turbulence load, as was the case with the Helios HP-03 aircraft. ITB also anticipated the turbulence load problem in the development of the HALE aircraf...
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| Format: | Dissertations |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/76332 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
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