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  2. Helicopter flight controls - Wikipedia

    en.wikipedia.org/wiki/Helicopter_flight_controls

    The collective pitch control, or collective lever, is normally located on the left side of the pilot's seat with an adjustable friction control to prevent inadvertent movement. The collective changes the pitch angle of all the main rotor blades collectively (i.e., all at the same time) and is independent of their position in the rotational cycle.

  3. Autorotation - Wikipedia

    en.wikipedia.org/wiki/Autorotation

    Raising the nose leads to more airflow through the rotor and raising the collective converts this airflow into more rotor lift which will slow the helicopter's forward speed. Raising the collective also keeps the rotor RPM from exceeding redline. Depending on the helicopter, before airspeed has completely decayed, the helicopter is leveled.

  4. Servo transparency - Wikipedia

    en.wikipedia.org/wiki/Servo_transparency

    A helicopter's main rotor hub. The vertical rods are at the end of the control chain that starts with the pilot controls. Helicopter flight controls are connected to the main and tail rotors, and include a cyclic stick, broadly to control forward-aft and left-right movements, a collective lever, broadly to control vertical movements, and anti-torque pedals, to control left and right yaw.

  5. Helicopter - Wikipedia

    en.wikipedia.org/wiki/Helicopter

    A helicopter has four flight control inputs. These are the cyclic, the collective, the anti-torque foot pedals, and the throttle. The cyclic control is usually located between the pilot's legs and is commonly called the cyclic stick or just cyclic or stick and moves forwards and backwards and side to side.

  6. Swashplate (aeronautics) - Wikipedia

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

    To control the collective pitch of the main rotor blades, the entire swashplate must be moved up or down along its axis without changing the orientation of the cyclic controls. Conventionally, each control mechanism, (roll, pitch, and collective) had an individual actuator responsible for the movement.

  7. Investigation into deadly midair collision focuses on ...

    www.aol.com/investigation-deadly-midair...

    But helicopters generally are not permitted to fly above 200 feet near Reagan, under Federal Aviation Administration rules. Tim Loranger, an aviation attorney and former U.S. Marine Corps aircraft ...

  8. Cyclic/collective pitch mixing - Wikipedia

    en.wikipedia.org/wiki/Cyclic/collective_pitch_mixing

    Cyclic/collective pitch mixing (CCPM) is a control concept employed in collective pitch radio-controlled helicopters. [1] CCPM reduces mechanical complexity and increases precision of control of the helicopter rotor's swashplate. Unlike conventional systems in which a single actuator is responsible for a single axis, CCPM mechanisms allow ...

  9. Remains of all D.C. plane crash victims recovered - AOL

    www.aol.com/more-wreckage-d-c-plane-153333545.html

    Remains from all 67 victims of the midair collision over Washington, D.C., that sent an American Airlines regional plane and an Army Black Hawk helicopter crashing into the Potomac River have been ...