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Journals / International Journal of 3D Printing Technologies and Digital Industry / 2022 / Cilt: 6 - Sayı: 1

AN EXPERIMENTAL DETERMINATION AND NUMERICAL ANALYSIS OF A LOITER MUNITION UNMANNED AERIAL VEHICLE SYSTEM

Ahmet Devlet Özçelik
Tamer Saraçyakupoğlu
Heyzem Doğukan Delibaş
Pages
83–101
Publication Date
2022-10-19
DOI
—
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AI Summary & Key Takeaways

AI Insight
⚡ TL;DR(Too Long; Didn't Read)

As a consequence of this research, it can be claimed that the UAV's mid-wing, twin-tail, and relatively light body will have three axis stability and offer numerous benefits, particularly in terms of operational cost.

📌 3 Key Takeaways

🎯
Objective & Hypothesis:This paper experimentally determinates the calculation of an Unmanned Aerial Vehicle (UAV) and analyzes the design criteria within four different scenarios.
📊
Key Findings & Data:The UAV may be operable day and night conditions, capable of 2-3 hours of flight hours, and will be launched from a catapult.
💡
Conclusion & Impact:As a consequence of this research, it can be claimed that the UAV's mid-wing, twin-tail, and relatively light body will have three axis stability and offer numerous benefits, particularly in terms of operational cost.
🔬Design:Research Article
📍Scope:Comprehensive Sample
⚙️Variables:Mission Profile · Speed Condition · Weight Calculation

Abstract

This paper experimentally determinates the calculation of an Unmanned Aerial Vehicle (UAV) and analyzes the design criteria within four different scenarios. The UAV to be designed is a loiter munition UAV system. A mobile or equipment such as a parachute and/or airbag. The UAV may be operable day and night conditions, capable of 2-3 hours of flight hours, and will be launched from a catapult. The UAV navigation system is compact and easily controlled by a personal Global Positioning System (GPS). The mentioned UAV will have a vast operational capability, especially for defense and border security activities since it is equipped with advanced avionics and a small physical footprint for covert operations. As a consequence of this research, it can be claimed that the UAV's mid-wing, twin-tail, and relatively light body will have three axis stability and offer numerous benefits, particularly in terms of operational cost.

Özet

This paper experimentally determinates the calculation of an Unmanned Aerial Vehicle (UAV) and analyzes the design criteria within four different scenarios. The UAV to be designed is a loiter munition UAV system. A mobile or equipment such as a parachute and/or airbag. The UAV may be operable day and night conditions, capable of 2-3 hours of flight hours, and will be launched from a catapult. The UAV navigation system is compact and easily controlled by a personal Global Positioning System (GPS). The mentioned UAV will have a vast operational capability, especially for defense and border security activities since it is equipped with advanced avionics and a small physical footprint for covert operations. As a consequence of this research, it can be claimed that the UAV's mid-wing, twin-tail, and relatively light body will have three axis stability and offer numerous benefits, particularly in terms of operational cost.

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Cite This Article

Özçelik, A. D., Saraçyakupoğlu, T., Delibaş, H. D. (2022). AN EXPERIMENTAL DETERMINATION AND NUMERICAL ANALYSIS OF A LOITER MUNITION UNMANNED AERIAL VEHICLE SYSTEM. International Journal of 3D Printing Technologies and Digital Industry, Cilt: 6 - Sayı: 1, 83–101. https://ajindex.com/articles/539726

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