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Open access Jul 2026

Gong-H: Design, Analysis and Control of a Tilt Trirotor Aircraft with Tandem Wings

Vertical take-off and landing (VTOL) configurations incur a structural weight penalty that reduces payload fraction and endurance compared to conventional fixed-wing and multirotor aircraft of comparable gross weight. To extend the endurance of VTOL UAVs, this work presents the design, analysis and control of a novel u...

Zemin Lin, Yi Zeng, Shi Lian et al. · 0 citations

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