Pitch Control

Pitch Control refers to the process of controlling the angle of an aircraft's nose up or down in relation to the horizon. It is one of the three primary axes of control in aviation, along with roll and yaw. Pitch control is achieved through the use of the aircraft's elevators, which are located on the trailing edge of the horizontal stabilizer. By changing the angle of the elevators, the pilot can adjust the pitch of the aircraft. Pitch control is essential for maintaining altitude, climbing, and descending during flight.

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Pitch Control

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