๐ซFlight Controls are divided into two main categories
๐ซPrimary Flight Control Systems
-AILERONS AND FLAPERONS
-SPOILERS AND SPEEDBRAKES
-ELEVATORS
-HORIZONTAL STABILIZER
-RUDDER.
๐ซHigh Lift Control systems
-TRAILING EDGE FLAPS
-LEADING EDGE SLATS
-KRUEGER FLAPS
๐ซPurpose of the primary flight control system (PFCS)- It controls the airplane flight attitude in relation to the three basic axes:
- Longitudinal (roll axis)
- Lateral (pitch axis)
- Vertical (yaw axis)
๐ซRoll Control- the roll control uses the ailerons, flaperons, and spoilers to control the airplane attitude about the longitudinal axis. During a bank of the airplane, the aileron and flaperon on one wing move in an opposite direction from the aileron and flaperon on the other wing.
๐ซPitch Control- The pitch control uses the horizontal stabilizer and the elevator to control the airplane attitude about the lateral axis.
๐ซYaw Control- The yaw control uses the rudder to control the airplane attitude about the vertical axis. The rudder has a tab which moves to increase the effectiveness of the rudder.
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