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  2. 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.

  3. Aircraft principal axes - Wikipedia

    en.wikipedia.org/wiki/Aircraft_principal_axes

    The yaw axis has its origin at the center of gravity and is directed towards the bottom of the aircraft, perpendicular to the wings and to the fuselage reference line. Motion about this axis is called yaw. A positive yawing motion moves the nose of the aircraft to the right. [1] [2] The rudder is the primary control of yaw. [3]

  4. 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.

  5. Rutan Defiant - Wikipedia

    en.wikipedia.org/wiki/Rutan_Defiant

    The main gear is fixed, and there are no flaps. The Propellers are fixed-pitch non-feathering, [3] which is unusual in a twin-engine design. Cockpit entry is through a side hinged canopy. [1] The winglets provide yaw stability. [3] Unusually, the Defiant has a ventral, port offset, forward mounted rudder, as can be seen in pictures of the plane ...

  6. Flight control surfaces - Wikipedia

    en.wikipedia.org/wiki/Flight_control_surfaces

    The rudder is a fundamental control surface which is typically controlled by pedals rather than at the stick. It is the primary means of controlling yaw—the rotation of an airplane about its vertical axis. The rudder may also be called upon to counter-act the adverse yaw produced by the roll-control surfaces.

  7. Stabilizer (aeronautics) - Wikipedia

    en.wikipedia.org/wiki/Stabilizer_(aeronautics)

    A Boeing 737 uses an adjustable stabilizer, moved by a jackscrew, to provide the required pitch trim forces. Generic stabilizer illustrated. A horizontal stabilizer is used to maintain the aircraft in longitudinal balance, or trim: [3] it exerts a vertical force at a distance so the summation of pitch moments about the center of gravity is zero. [4]

  8. What is airplane mode, anyway? 5 travel questions about ... - AOL

    www.aol.com/airplane-mode-anyway-5-travel...

    It's a lot more vital than keeping your phone in airplane mode. In the past five years, the number of fires related to lithium-ion batteries has jumped over 40% , according to a CBS News analysis ...

  9. Flying wing - Wikipedia

    en.wikipedia.org/wiki/Flying_wing

    Moreover, solutions may produce a final design that is still too unsafe for certain uses, such as commercial aviation. Further difficulties arise from the problem of fitting the pilot, engines, flight equipment, and payload all within the depth of the wing section. Other known problems with the flying wing design relate to pitch and yaw.