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...
Aviation Science and Knowledge