Configuration method for man-machine interactive airplane mission payload

The invention discloses a configuration method for man-machine interactive airplane mission payload, and belongs to the field of airplane weight engineering. The configuration method comprises the following steps: configuring an oil consumption rule: selecting a corresponding oil consumption rule by aiming at different mission configurations; configuring effective payload: according to mission requirements, assigning an effective payload type for the specific position of the airplane; virtualizing fuel consumption: simulating the change of the weight, the center of gravity and the rotation inertia of the airplane in a fuel consumption process; virtualizing payload consumption: under the state of airplane assigned excess oil, simulating the change situation of the weight, the center of gravity and the rotation inertia during effective payload consumption (such as weapon put/emission). The configuration method has the advantages that the technical scheme can virtualize the payload put/emission on the basis of the center of gravity and the fuel consumption curve of the airplane to precisely calculate the weight, the center of gravity and the rotation inertia of the airplane in real time, and estimate the change range of the center of gravity of the airplane, and therefore, a problem that the change range of the center of gravity of the airplane only can be roughly estimated with a traditional means is solved.