SONGBIRD – AN INNOVATIVE UAS COMBINING THE ADVANTAGES OF FIXED WING AND MULTI ROTOR UAS

10 citations as recorded by crossref.

1. Vertical Take-off and Landing Unmanned Aerial Vehicle Design Based on Foam 3D Printing Technology W. Sun & N. Zhao 10.1109/ACCESS.2024.3506597
2. Fast Hildreth-based Model Predictive Control of Roll Angle for a Fixed-Wing UAV V. Lam et al. 10.1016/j.ifacol.2020.12.1608
3. A method for evaluating the wind disturbance rejection capability of a hybrid UAV in the quadrotor mode H. Zhang et al. 10.1177/1756829319869647
4. Mounting RIS Panels on Tethered and Untethered UAVs: A Survey A. Nazar et al. 10.1007/s13369-023-08603-0
5. A Survey: Flight Mechanism and Mechanical Structure of the UAV C. Lee et al. 10.1007/s12541-021-00489-y
6. Micro aerial vehicle with basic risk of operation A. de Lucena et al. 10.1038/s41598-022-17014-4
7. Applications and classifications of unmanned aerial vehicles: A literature review with focus on multi-rotors M. Sabour et al. 10.1017/aer.2022.75
8. Mapping of Archaeological Sites using UAV Aerial Survey and PPK GNSS Ground Survey Techniques in Central Asia S. Suab et al. 10.1088/1755-1315/540/1/012014
9. Double Hybrid Tailsitter Unmanned Aerial Vehicle With Vertical Takeoff and Landing A. De Lucena et al. 10.1109/ACCESS.2022.3161490
10. Safety Systems for Emergency Landing of Civilian Unmanned Aerial Vehicles (UAVs)—A Comprehensive Review M. Farajijalal et al. 10.3390/drones9020141