Abstract:
This project study the condition of twin engine air craft during takeoff , at one engine failure ,This causes several negative effects on A/C, in addition to the loss of engine thrust ,the performance and stability are changes.
A simple ,uncomplicated ,high resolution system has been proposed ,operating automatically without outside interference , where it works to determine the balance of the plane when the malfunction occurs, calculated the angles of the required control surfaces and execute the desired for balance of A/C , the angles and moments required for the plane equilibrium was calculated by scientific steps, computer applications were used to explain the relation between the variables required to operation of the system the results of the calculations were acceptable in comparison to the results required for the balance of the aircraft
