Pedal: A flight control operated by pushing with feet, primarily to control yaw via the rudder in fixed-wing aircraft or thrust to tail rotor in rotary-wing aircraft; pedals are automatically controlled in modern aircraft.
Pedals: These are not rudder pedals, although they are in the same place as rudder pedals on an airplane. A single rotor helicopter has no real rudder.
Rudder pedals, which control rotation of the aircraft about the yaw axis. There are two pedals that pivot so that when one is pressed forward the other moves backward, and vice versa.
4. Rudder Pedals :
Front - Located on left and right forward of floor board and are conventional. They are toe type pedals.
Rear - Located to left and right of front seat.
Stuck Pedals (fixed pitch failures)
A fixed pitch failure of the tail rotor is one kind of failure, but we tend to charactersize it as stuck left, stuck right, or stuck neutral.
Antitorque pedals enable the pilot to compensate for torque variance. A significant part of the engine power is required to drive the tail rotor, especially during operations when maximum power is used.
This symmetry reduces the demands on the pilot in coordinating the cyclic, collective and pedals. In addition, it results in a power to weight ration that is approximately 15% better than the single rotor.
The nosewheel strut is steerable, with direct linkage to the rudder pedals, and uses a single heavy-duty bungee for shock absorbency.
That is, you are steadily pushing on the right rudder pedal. Then the slip/roll coupling (as discussed in section 9.1 and section 9.2) will cause it to spin to the right.
Steering, while on the ground, is done with the rudder pedals. If the airplane begins to move to the left, lightly apply right rudder pressure to stop the leftward movement.
Rudder-pedal action is smooth and positive, with ample feedback in flight. Same on the ground, in fact, thanks to the steerable nosewheel. Keeping the J230 coordinated was easy.
Turning the rudder trim knob changes the tension on a spring connected to the rudder pedal torque tubes. In other words, the trim knob changes the relative positions of the rudder pedals instead of adjusting a tab on the rudder itself.
rudder - A control surface on the trailing edge of the vertical part of the tail that is used to make the aircraft yaw. The rudder is controlled by rudder pedals. Pushing the left rudder pedal will tilt the rudder to the left.
as did Le Sauteral's 1923 pedal-powered machine (built in 1923)
and the 1910 design (snow), which was based on a discarded (but theoretically feasible) Cayley idea.
The primary flight controls are the wheel, yoke, cyclic, pedals, throttle, and collective. Secondary flight controls are flight controls that are not primary and include the flaps, slats, stabilizer, and landing gear.
Rudder and aileron trim tabs operate on the same principle as the elevator trim tab to relieve pressure on the rudder pedals and side ward pressure on the control wheel, respectively.
Hovercraft - ...
One machine consisted of an enclosed cabin in which a man's pedalling with both arms and legs would be amplified by gears and transferred to the flapping wings outside. A machine that flies by flapping its wings became known as a ornithopter.
Throttle The control that allows the pilot to change the speed of the engine. In a car, the "gas pedal" is actually the throttle control for the car.
Once aligned on the runway, steering the aircraft is normally accomplished by using foot pedals that manipulate the nose wheel until the speed is sufficient enough that wind rushing by the rudder on the aircraft tail makes nose wheel steering ...
JOYSTICK - A single floor- or roof-mounted control stick"sideways movement produces ROLL, and forward/backward movement produces PITCH (rudder pedals produce YAW).
Forces the tail left or right, correspondingly "yawing" the aircraft right or left. Rudder movement "coordinates" with the banking of wings to balance a turn. Controlled by left and right rudder (foot) pedals.
 See also: Pilot, Flight, Aircraft, Power, Speed
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