Kimathi S, Lantos B. Modelling and Attitude Control of an Agile Fixed Wing UAV based on Nonlinear Dynamic Inversion. Period. Polytech. Elec. Eng. Comp. Sci. [Internet]. 2022 Jan. 1 [cited 2024 Jul. 3];66(3):227-35. Available from: https://pp.bme.hu/eecs/article/view/20287