Flight Stability And Automatic Control Nelson Solutions -
Therefore, the aircraft is laterally stable.
∂n / ∂β > 0
where m is the pitching moment and α is the angle of attack. Flight Stability And Automatic Control Nelson Solutions
Altitude Sensor → Controller → Actuator → Aircraft → Altitude Sensor Therefore, the aircraft is laterally stable
For longitudinal stability, the following condition must be satisfied: the following condition must be satisfied:
