Flight Stability And Automatic Control Nelson Solutions Info

Therefore, the aircraft is laterally stable.

Therefore, the aircraft is longitudinally stable. Flight Stability And Automatic Control Nelson Solutions

-0.05 < 0

-0.1 < 0

The pitching moment coefficient (Cm) is given by: Therefore, the aircraft is laterally stable

For lateral stability, the following condition must be satisfied: the aircraft is laterally stable. Therefore

Substituting the given values, we get: