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Propulsion Requirement and Analysis of a Canard Prandtl – Wing Unmanned Aerial Vehicle Platform for Civilian-Oriented Missions

Year: 2024

Type: conference-paper

Abstract: This study evaluated the propulsion performance of a canard Prandtl-wing unmanned aerial vehicle (UAV) using computational methods to assess its compliance with mission requirements.The UAV specifications included a takeoff gross weight of 7 kgf, a cruising speed of 20 m/s, and a minimum endurance of 1 hour.Analysis revealed that maximum power consumption occurred during takeoff, requiring 66.48 N of thrust and 200 W power after 2 minutes.During the loiter phase, the system achieved minimum power consumption of 60 W with 51 N of thrust at 16 m/s.Descent commenced at 11.5 minutes, with a descent and landing phase lasting 3.5 minutes.Power consumption decreased during this phase, completing the mission in 15 minutes.The 15-minute sample flight plan, covering 2.5 km, was scaled up to a 1-hour flight at 10 km, proving the electric propulsion system's capability to meet the design specifications for civilian oriented missions.

Source: Proceedings of International Exchange and Innovation Conference on Engineering & Sciences (IEICES)

DOI: 10.5109/7323282

Authors: Cindy May C. Belivestre, Jonathan C. Maglasang

Institutions: Caraga State University, Mindanao State University – Iligan Institute of Technology, Cebu Technological University

Language: English

Topic: Advanced Aircraft Design and Technologies

Subfield: Global and Planetary Change

Field: Environmental Science

Domain: Physical Sciences

Open Access status: hybrid

OpenAlex ID: W4404653686

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