Dimitrios E. Mazarakos Mechanical Engineering and Aeronautics, University of Patras, Greece Email: dmazarak.upatras@gmail.com
Abstract
This paper presents a mathematical model for a scaled planetary UAV, considering fundamental flight paths—climb, cruise, and turn. The research introduces an earth-flight test model for simulation purposes, demonstrating the importance of planetary exploration and communication systems. A scaling method is proposed, integrating atmospheric conditions, velocity, and propulsion constraints. The updated design calculations provide a structured framework for UAV testing in terrestrial conditions, aiding early-stage functional system evaluations.
Keywords
Aerodynamics, Scaling Laws, High-Speed UAV, Solar Planetary Missions
How to Cite
Dimitrios E. Mazarakos, “Flight Mechanics & Scaling Laws Method in UAV Design for Solar Planetary Missions,”
International Journal of Engineering and Techniques, Volume 9, Issue 4, 2023. ISSN 2395-1303
Post Comment