Stick Deflection Angle Given By Stick Force Calculator

In flight mechanics, stick deflection angle refers to the angular displacement of the control stick or yoke in an aircraft cockpit. It represents the physical movement of the control input device by the pilot, influencing the corresponding deflection of control surfaces such as ailerons, elevators, or rudders. The stick deflection angle is a crucial parameter in understanding and analyzing the pilot’s input and its impact on the aircraft’s attitude and control. The formula to calculate stick deflection angle as follows:

• δ_e​ is the Elevator Deflection Angle in radian,
• H_e is the Hinge Moment in Nm,
• l_s is the Stick Length​ in m
• δ_s​ is the Stick Deflection Angle in radian,
• F is the Stick force in N.