Flight Stability And Automatic Control Nelson Solutions

Therefore, the aircraft is laterally stable.

Cm = ∂m / ∂α

: Mathematical quantifications of how aerodynamic forces change with variables like the angle of attack. Oscillation Damping Flight Stability And Automatic Control Nelson Solutions

and how the tail creates restoring moments to keep the nose where it belongs. Equations of Motion (Chapter 3): Therefore, the aircraft is laterally stable