In helicopters, yaw is controlled through the pedals, which alter the angle of attack of the tail rotor blades.
En los helicópteros, la guiñada se controla a través de los pedales, que alteran el ángulo de ataque de las palas del rotor de cola.
In helicopters, the cyclic controls the tilt of the main rotor, producing pitch and roll.
En los helicópteros, el cíclico controla la inclinación del rotor principal, produciendo cabeceo y balanceo.
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