Helicopter flight controls are used to achieve and maintain controlled aerodynamic helicopter flight. Changes to the aircraft flight control system transmit mechanically to the rotor, producing aerodynamic effects on the rotor blades that make the helicopter move in a desired way. To tilt forward and back (pitch) or sideways (roll) requires that the controls alter the angle of attack of the main rotor blades cyclically during rotation, creating differing amounts of lift at different points in the cycle. To increase or decrease overall lift requires that the controls alter the angle of attack for all blades collectively by equal amounts at the same time, resulting in ascent, descent, acceleration and deceleration.
A typical helicopter has three flight control inputs: the cyclic stick, the c...
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Eurocopter EC-145 Cockpit Controls HeliRussia 2008 (62-39).jpg
Eurocopter EC 145
Guimbal Cabri G2 1003 cockpit 2.jpg
Guimbal Cabri G2 Cockpit 2
Helicopter Collective.gif
When the Collective is pulled, the rotor angle changes.
Helicopter Cyclic.gif
When the cyclic is pushed forwards, the rotor tilts
Helicopter Cyclic 2.gif
When the cyclic is pushed to the side, the rotor tilts to the side
Helicopter controls diagram.svg
Helicopter controls diagram
Helicopter tail rotor pedals.gif
The tail rotor is operated with the pedals
People icon.svg
People icon
Robinson R22 Cockpit-001.jpg
The cockpit of a Robinson R22 Helicopter
Pilatus Agusta A109 Flug.jpg
A rescue helicopter type Agusta A109K2 leaves Mount Pilatus after recovering a patient.