When the pilot moves the cyclic control, the lower swash plate tilts, causing the upper swash plate and rotor blades to tilt in the same direction. This causes the helicopter to move in the direction of the tilt. When the pilot moves the collective control, both swash plates tilt in the same direction, causing all of the rotor blades to tilt in the same direction. This causes the helicopter to climb or descend. When the pilot moves the tail rotor control, the upper swash plate tilts in one direction while the lower swash plate tilts in the opposite direction. This causes the rotor blades to tilt in such a way that the helicopter turns around its vertical axis.