At the outer ends of the wings are 'ailerons'. These are like flaps, but when one goes up, the other goes down, thus the aircraft rolls.
The coordinated pair of ailerons does.
Aircraft are able to turn left to right, vice versa or around by controlling the spin of the wheels. Preventing the right wheels to roll will turn the aircraft to right and controlling the left wheels will make a left turn.
Operating the ailerons will cause the aircraft to roll.
Kempton H. Roll has written: 'Controlling corrosive air pollutants'
Elevators control the pitch (up and down) of the aircraft. Ailerons control the roll of the aircraft. And rudders control the yaw of the aircraft.
That is when the aircraft rotates around it's axis.
ON a slanted surface
on a smooth surface
A ball rolling along any surface will be slowed by friction. Different materials used for the ball and the rolling surface will affect the distance a ball will roll but in general, the smoother and more polished the surface is, the further a ball will roll.
Dutch roll is the tendency of an aircraft to roll and yaw about its longitudinal and vertical axis due to inherent instability in the design of the aircraft. Generally it is the result of a small vertical stabilizer design.
Pitch is a rotating movement of the body of the aircraft about the axis of the wings. Pitch is represented by rotating to tilt the aircraft up or down. Yaw is a rotation left and right, similar to turning your head to the left and right. Roll is a rotation of the aircraft about the front to rear axis. An aircraft would roll if the pilot wanted to turn it to fly upside down.
Roll, pitch, and yaw - flight dynamics. See the below link for more info.