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  2. File:MISB ST 0601.8 - Yaw, Pitch & Roll.png - Wikipedia

    en.wikipedia.org/wiki/File:MISB_ST_0601.8_-_Yaw...

    It is recommended to name the SVG file “MISB ST 0601.8 - Yaw, Pitch & Roll.svg”—then the template Vector version available (or Vva) does not need the new image name parameter. Summary Description MISB ST 0601.8 - Yaw, Pitch & Roll.png

  3. File:Yaw Axis Corrected.svg - Wikipedia

    en.wikipedia.org/wiki/File:Yaw_Axis_Corrected.svg

    This image is a derivative work of the following images: File:Yaw_Axis.svg licensed with Cc-by-sa-3.0 ... Diagram showing Yaw, Pitch and Roll movements of aircraft in ...

  4. File:Roll pitch yaw mnemonic.svg - Wikipedia

    en.wikipedia.org/wiki/File:Roll_pitch_yaw...

    You are free: to share – to copy, distribute and transmit the work; to remix – to adapt the work; Under the following conditions: attribution – You must give appropriate credit, provide a link to the license, and indicate if changes were made.

  5. Aircraft principal axes - Wikipedia

    en.wikipedia.org/wiki/Aircraft_principal_axes

    The position of all three axes, with the right-hand rule for describing the angle of its rotations. An aircraft in flight is free to rotate in three dimensions: yaw, nose left or right about an axis running up and down; pitch, nose up or down about an axis running from wing to wing; and roll, rotation about an axis running from nose to tail.

  6. Aircraft flight dynamics - Wikipedia

    en.wikipedia.org/wiki/Aircraft_flight_dynamics

    With a symmetrical rocket or missile, the directional stability in yaw is the same as the pitch stability; it resembles the short period pitch oscillation, with yaw plane equivalents to the pitch plane stability derivatives. For this reason, pitch and yaw directional stability are collectively known as the "weathercock" stability of the missile.

  7. Spacecraft flight dynamics - Wikipedia

    en.wikipedia.org/wiki/Spacecraft_flight_dynamics

    The three principal moments of inertia I x, I y, and I z about the roll, pitch and yaw axes, are determined through the vehicle's center of mass. The control torque for a launch vehicle is sometimes provided aerodynamically by movable fins, and usually by mounting the engines on gimbals to vector the thrust around the center of mass.

  8. Six degrees of freedom - Wikipedia

    en.wikipedia.org/wiki/Six_degrees_of_freedom

    First-person shooter (FPS) games generally provide five degrees of freedom: forwards/backwards, slide left/right, up/down (jump/crouch/lie), yaw (turn left/right), and pitch (look up/down). If the game allows leaning control, then some consider it a sixth DOF; however, this may not be completely accurate, as a lean is a limited partial rotation.

  9. Flight dynamics - Wikipedia

    en.wikipedia.org/wiki/Flight_dynamics

    Yaw is known as "heading". A fixed-wing aircraft increases or decreases the lift generated by the wings when it pitches nose up or down by increasing or decreasing the angle of attack (AOA). The roll angle is also known as bank angle on a fixed-wing aircraft, which usually "banks" to change the horizontal direction of flight.