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https://repositori.uma.ac.id/handle/123456789/30929| Title: | Analisis Pengaruh Hubungan Penambahan Beban Terhadap Karakteristik Terbang Dan Ketinggian Drone E88 Pro |
| Other Titles: | Analysis of the Effect of Added Load on the Flight Characteristics and Altitude of the E88 Pro Drone |
| Authors: | Dhillon, Dhalveer Singh |
| metadata.dc.contributor.advisor: | Aldori, Yopan |
| Keywords: | Penambahan Beban;Krakteristik Terbang;Drone E88 PRO;Flight Characteristics;Additional Load |
| Issue Date: | 28-Mar-2026 |
| Publisher: | Universitas Medan Area |
| Series/Report no.: | NPM;218130055 |
| Abstract: | Penambahan beban berpengaruh terhadap kemampuan drone dalam mempertahankan ketinggian. Pada beban standar (massa total 77,79 g) dan penambahan 10 g (massa total 87,79 g), drone masih mampu mempertahankan ketinggian target 1 meter. Mulai dari penambahan 20 g (massa total 97,79 g), ketinggian rata-rata turun menjadi 0,75–0,82 m. Pada penambahan 30 g (massa total 107,79 g), ketinggian turun menjadi rata-rata 0,56–0,58 m. Sedangkan pada beban 40 g dan 50 g (massa total 117,79–127,79 g), drone gagal mempertahankan ketinggian (jatuh ke lantai) meskipun dapat kembali terbang setelah peningkatan kecepatan motor secara manual, namun drone sudah sulit untuk dikendalikan dan kehilangan kestabilan pada beban tersebut. Koefisien lift (Cl) bersifat konstan pada nilai 0,33098 untuk semua variasi beban. Hal ini menunjukkan bahwa motor brushed dan propeller drone E88 Pro tidak mampu meningkatkan koefisien lift secara signifikan untuk mengimbangi penambahan massa. Sementara itu, koefisien drag (Cd) mengalami penurunan dari 0,016 menjadi 0,014 seiring bertambahnya beban, namun drag total justru meningkat karena massa yang lebih besar. Penambahan beban menyebabkan penurunan waktu hovering pada drone. Waktu terbang maksimum pada kondisi tanpa beban tambahan mencapai rata-rata 633 detik (≈10,5 menit), sedangkan pada beban 50 g waktu terbang turun menjadi rata-rata 365 detik (≈6 menit). Penurunan ini disebabkan oleh kebutuhan thrust yang lebih tinggi sehingga konsumsi daya baterai 3,7 V 1800 mAh menjadi lebih boros. Increasing the load affects the drone's ability to maintain altitude. At the standard load (total mass of 77.79 g) and with an added 10 g (total mass of 87.79 g), the drone is still able to maintain the target altitude of 1 meter. Starting with an added load of 20 g (total mass of 97.79 g), the average altitude drops to 0.75–0.82 m. With an added load of 30 g (total mass of 107.79 g), the altitude falls to an average of 0.56–0.58 m. Meanwhile, at loads of 40 g and 50 g (total mass of 117.79–127.79 g), the drone fails to maintain altitude (falling to the floor); although it can resume flight after manually increasing motor speed, it becomes difficult to control and loses stability at these loads. The lift coefficient (Cl) remains constant at 0.33098 across all load variations. This indicates that the E88 Pro drone's brushed motors and propellers are unable to significantly increase the lift coefficient to compensate for the added mass. Meanwhile, the drag coefficient (Cd) decreases from 0.016 to 0.014 as the load increases, yet total drag rises due to the greater mass. Adding load results in reduced hovering time for the drone. The maximum flight time without additional load averages 633 seconds (≈10.5 minutes), whereas with a 50 g load, the flight time drops to an average of 365 seconds (≈6 minutes). This reduction is caused by the need for higher thrust, leading to increased power consumption from the 3.7 V 1800 mAh battery. |
| Description: | 51 Halaman |
| URI: | https://repositori.uma.ac.id/handle/123456789/30929 |
| Appears in Collections: | SP - Mechanical Engineering |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| 218130055 - Dhalveer Singh Dhillon - Fulltext.pdf | Cover, Abstract, Chapter I, II, III, V, Bibliography | 1.44 MB | Adobe PDF | View/Open |
| 218130055 - Dhalveer Singh Dhillon - Chapter IV.pdf Restricted Access | Chapter IV | 2.14 MB | Adobe PDF | View/Open Request a copy |
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