Load identification-based high aspect ratio wing load real-time monitoring method

The invention discloses a high aspect ratio wing load real-time monitoring method based on load identification, and the method mainly comprises the steps: (1) arranging a strain bridge at the related position of a wing according to the load measurement requirement; (2) performing a static load calibration test and a dynamic load calibration test on the wing which is additionally provided with the strain bridge in a ground calibration mode to obtain a static load calibration matrix and a dynamic load calibration matrix; and (3) simulating the load borne by the aircraft in a flight state by means of a wind tunnel test, and monitoring the static and dynamic loads borne by the wing in real time by combining static and dynamic strain data separated from the actually measured strain data with the static and dynamic load calibration matrix. The invention provides the real-time monitoring method for the load borne by the high-aspect-ratio wing under the condition that the existence of the structural inertia force is