Control Accuracy Calculation of Flap & Slat System of Civil Aircraft

The control accuracy of the flap & slat system of civil aircraft greatly affects the actual theoretical position of the flap & slat surface, which influences the aircraft’s ability to gain lift and the design of the structural stop block. Therefore, it is important to analyze the origins of the accuracy components to improve the control accuracy of the system. This paper introduces how the control accuracy of the flap & slat system affects the aircraft, analyzes each main factor of the system control accuracy and makes a specific analysis of its origins, and finally proposes a method based on the self-compensating balance of the computer to improve the control accuracy of the system. It is believed that this study is of great significance for the design of domestic large aircraft design related.