System and method for the determination of local accelerations, dynamic load distributions and aerodynamic data the case of an aircraft

摘要

The present invention provides a method and a system (1) to the integrated determination of aerodynamic data, dynamic load distributions and local accelerations in the case of an aircraft, in particular in the case of an aircraft, during the flight. On the aircraft are sensors (2) for the direct and indirect detection of aerodynamic parameters, local accelerations and / or structural loads of the aircraft is provided. A in the aircraft or provided in the ground station calculation unit (3) calculated on the basis of a not - linear simulation model of the aircraft the aerodynamic data, local accelerations and dynamic load distributions of the aircraft in a function of the acquired aerodynamic parameters of the aircraft. The calculation can be done in real time.