Difference Between Yaw and Pitch

February 2022 · 5 minute read

Aircraft are vehicles that operate in all three dimensions of practical existence due to which, the stability and control are highly complex. The movement of aircraft in each of these three dimensions is identified as yaw, pitch, and roll. While the components of these movements are similar including velocity, angle, and torque, etc., they largely differ in their directions.

Yaw vs Pitch

The main difference between yaw and pitch is that yaw is the movement of a vehicle around the vertical axis whereas pitch is the movement of a vehicle around the lateral axis. The two movements can be calculated for the same vehicle and are perpendicular to each other.

Yaw refers to the twisting, rotating, of vehicles that operate in three dimensions around the vertical axis. These vehicles include ships, airplanes, and satellites, etc. The up and down axis is the vertical axis, which controls the yaw movement.

Pitch refers to the twisting, rotating, of vehicles that operate in three dimensions around a side-to-side or lateral axis. Like yaw, these vehicles include ships, airplanes, satellites, etc. The left and right axis is the lateral axis, which controls the pitch movement.

Comparison Table Between Yaw and Pitch

Parameters of ComparisonYawPitch
AxisVertical Axis.Lateral Axis.
DirectionIts direction is left and right.Its direction is up and down.
ControlIt is controlled by the rudder.It is controlled by the elevator.
AngleYaw angle is denoted by Psi.Pitch angle is denoted by Theta.
MnemonicIts mnemonic is the word ‘Door’.Its mnemonic is the word ‘Pitcher’

What is Yaw?

Yaw refers to the twisting, rotating, of vehicles that operate in three dimensions around a vertical axis. These vehicles include ships, airplanes, and satellites, etc. The up and down axis is the vertical axis, which controls the yaw movement. The yaw rate of the vehicle is the angular velocity of the rotation when the vehicle is rotating about the vertical axis.

In airplanes, yaw movement is controlled by the rudder, which is the yaw control surface of vehicles that operate in three dimensions. On a vertical tail fin known as the vertical stabilizer in an airplane, the rudder repositions from sides, which pushes the tail left or right. The airplane’s pilot controls the rudder along with the ailerons to turn the airplane in a specific direction. Scientifically, this yaw movement is the component of torque about the vertical axis.

The yaw rate in a vehicle can be measured by installing accelerometers in the vertical axis. Such measuring devices are collectively known as yaw rate sensors. Additionally, the yaw velocity is measured with the help of gyroscopes.

As understanding, the yaw movement is often confusing, the mnemonic to remember its direction is the word ‘Door’. Yaw movement is similar to the direction of opening or closing a door.

What is Pitch?

Pitch refers to the twisting, rotating, of vehicles that operate in three dimensions around a side-to-side or lateral axis. Like yaw, these vehicles include ships, airplanes, satellites, etc. The left and right axis is the lateral axis, which controls the pitch movement. The pitch rate of the vehicle is the angular velocity of the rotation when the vehicle is rotating about the lateral axis.

In airplanes, the pitch movement is controlled by the elevator, which is the pitch control surface of the vehicles that operate in three dimensions. On the horizontal tail surface, the elevator repositions through the upper and lower portion, which pushes the tail in up and down directions. The airplane’s pilot controls the elevator to turn the airplane in up and down directions. Scientifically, this pitch movement is the component of torque about the lateral axis.

The pitch movement and angle are calculated by installing an Attitude Indicator on the vehicle. Since the pitch movement is about the lateral axis, it directly decides the altitude of the flight and largely contributes to keeping the vehicle stable. The mnemonic to remember its direction is the word ‘Pitcher’. Pitch movement is similar to the direction of a liquid flowing out from a pitcher.

Main Differences Between Yaw and Pitch

  • Yaw is the movement around the vertical axis whereas pitch is the movement around the lateral axis.
  • Yaw movement decides the direction of the vehicle whereas pitch decides the altitude.
  • Yaw movement is measured by accelerometers whereas pitch is measured by attitude indicators.
  • The mnemonic to yaw’s direction is the direction of doors, whereas for pitch, it is the direction of the pitcher’s flow.
  • Yaw is controlled by the rudder whereas pitch is controlled by the elevator.
  • Conclusion

    The working of aircraft is far more complex than regular vehicles that move only around two axes. The existence of the third axis in the aircraft’s movement also causes an imbalance in the air. To control such imbalance and introduce stability, each movement in the three dimensions is identified as yaw, pitch, and roll.

    Theoretically, this phenomenon is imagined as three lines drawn on an airplane, signifying the axes. These three lines, called axes, are the airplane’s three dimensions of motion that intersect at the center of gravity. This balances the movement of aircraft. A pilot rotates the airplane around the center of gravity.

    When we talk about the three-axis, their components are similar including angle, velocity, torque, etc. However, the only significant difference between them is the direction of their movement. Yaw is controlled by the rudder, the pitch is controlled by the elevator, and the roll is controlled by ailerons.

    To master straight and level flight, pursuing pilots need to have a theoretical as well as the practical practice of the three movements. In more advanced maneuvers including airforce, balancing the three-axis requires the expertise of the science behind it. Hence, yaw, pitch, and roll make the conceptual base of pilots.

    References

  • https://www.sciencedirect.com/science/article/pii/S0360301606009734
  • https://ieeexplore.ieee.org/abstract/document/1188020/
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