Optimization of aircraft fuel supply based on centroid balance strategy

The centroid is a special point determined by the mass distribution of the object, which is an important intrinsic parameter. The centroid balance is the key technology to ensure the safe operation of the aircraft. However, the limitations of the internal system structure of the aircraft will affect the centroid position, as well as attitude changes and fuel consumption of the aircraft, so it is necessary to develop the corresponding centroid balancing strategy to ensure that the aircraft fully exerts its stability and maneuverability. Firstly, the centroid change curve is drawn based on greedy strategy and mixed integer quadratic programming in this study, then the strategic optimization calculation model that can accurately describe the oil supply problem is established. Finally, using Gurobi to obtain a high-quality feasible solution within the effective time and ensure the centroid balance of the aircraft.