Calculate Change of Angle of Attack

Calculate Change of Angle of Attack

Where

q = Pitching rate

L = Lift

V = Velocity

Angle of Attack (Δα) is the angle between the relative Air and Fuselage reference line (FRL).

To change Angle of Attack(Δα), we usually input elevator movements to increase or decrease the lift of the horizontal stabilizer

                                                                                                                                              Chandan Singh