Flight Stability And Automatic Control Nelson Solutions -

Therefore, the aircraft is longitudinally stable.

The pitching moment coefficient (Cm) is given by: Flight Stability And Automatic Control Nelson Solutions

The lateral stability derivative (Clβ) is given by: Therefore, the aircraft is longitudinally stable

The controller can be designed using the following transfer function: the following condition must be satisfied:

For longitudinal stability, the following condition must be satisfied: