MANUFAKTUR STRUKTUR PADA WING PESAWAT SKY LAB X-8

Fauzi Muhammad, Fattya (2024) MANUFAKTUR STRUKTUR PADA WING PESAWAT SKY LAB X-8. Skripsi thesis, Institut Teknologi Dirgantara Adisutjipto.

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Abstract

In the aviation industry, technological advances are increasingly in demand because of their ability to fly planes to take off and land vertically. UAVs, especially unmanned aerial vehicles (UAVs), are increasingly important in various applications such as environmental monitoring, mapping and surveillance. So the aim of the research that will be used is to determine a wing structure design that is suitable for sky lab aircraft when in the air for the purpose of delivering emergency supplies. Errors in planning can result in fatal errors in the design results. Then the method used is a simulation method to design or design the fixed wing structure of the Sky Lab aircraft so that we can find out whether or not the frame is suitable for construction. The test flight was carried out on September 16 2023, the aircraft took off well and safely, where in operation all components functioned well as expected. The Sky-Lab aircraft was declared a successful flight test with all control systems functioning normally.

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