06.2 - Flight Dynamics and Control (UAV related)

STABILITY ANALYSIS OF A LIGHT UAV WITH SOLAR PROPULSION

C. Galinski¹, T. Goetzendorf-Grabowski¹; ¹Warsaw University of Technology, Poland

The paper presents the results of research on an experimental solar-powered UAV. High flight stability and generally good handling characteristics are crucial because this aircraft is designed for precise measurements. The specific design, including a flat-top profile, unparalleled in other designs, and an unusual upper mass distribution, posed additional challenge. The paper presents the results of stability analysis on various configurations.

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DOI: 10.71945/icas2026_0219