2-s2.0-85104195789. (2021). UAV Dynamic Behaviour Comparison of Quadcopter Based on Thrust Differential and Tilted Rotor. Journal of Aeronautics, Astronautics and Aviation , 53(2), . https://doi.org/10.6125/JoAAA.202106_53(2).18
芝加哥风格引文2-s2.0-85104195789. "UAV Dynamic Behaviour Comparison of Quadcopter Based on Thrust Differential and Tilted Rotor." Journal of Aeronautics, Astronautics and Aviation 53, no. 2 (2021). https://doi.org/10.6125/JoAAA.202106_53(2).18.
MLA引文2-s2.0-85104195789. "UAV Dynamic Behaviour Comparison of Quadcopter Based on Thrust Differential and Tilted Rotor." Journal of Aeronautics, Astronautics and Aviation , vol. 53, no. 2, 2021, https://doi.org/10.6125/JoAAA.202106_53(2).18.
警告:这些引文格式不一定是100%准确.