When controlling pitch, which direction should the control column be moved to tilt upwards?

To tilt the aircraft upwards, the control column should be moved backward. This action causes the elevators on the tail of the aircraft to deflect upwards, increasing the angle of attack of the wings and resulting in an increase in lift. When lift exceeds weight, the aircraft will climb.

Moving the control column in a forward direction would have the opposite effect, causing the aircraft to pitch downwards. Similarly, moving the control column to the left or right primarily affects the roll of the aircraft, not the pitch. Understanding this fundamental concept of how control inputs relate to the aircraft's orientation is crucial for effective flying.