🚁 Helicopter Flight Physics Lab: Dissymmetry of Lift, Blade Flapping, Cyclic and Autorotation

Earth helicopter control lab: blade-element solution of dissymmetry of lift, hinged-blade flapping with its 90 degree phase lag, cyclic and collective trim, Glauert translational lift, the power curve with V_mp, tail-rotor torque balance and engine-out autorotation with flare. Different from the Mars/Titan rotorcraft lab and the helicopter rescue game: it solves the rotor aerodynamics themselves.