How does a standard quadcopter achieve yaw control (rotation around the vertical axis)? - EASA Drone A2 License - 23

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Home > Exam Questions > EASA Drone License A2 > Flight performance and planning > How does a standard quadcopter achieve yaw control (rotation around the vertical axis)?

Question 23 - Flight performance and planning - EASA Drone License A2

By tilting a physical tail rotor

By altering the speed of the clockwise-spinning motors relative to the counter-clockwise-spinning motors, creating a torque imbalance

By shifting the internal battery weight left or right

By using movable aerodynamic flaps on the arms

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