Due to the complex dynamic characteristics of aircraft fuel consumption, it is difficult to dynamically optimize the fuel filling amount in refueling truck fuel filling control, resulting in low matching between fuel filling control amount and filling amount, and poor control accuracy. Design an intelligent fuel injection control method for aircraft tank refueling vehicles that considers fuel filling volume. To comprehensively capture the complex dynamic characteristics of aircraft fuel consumption, LSTM model, CNN model, and Transformer model are combined to implement aircraft fuel consumption prediction; Based on the predicted fuel consumption of the aircraft, the aircraft"s fuel filling amount is dynamically calculated by combining the amount of fuel required for ground taxiing, the amount of fuel required for flying to an alternate airport, and the amount of unexpected fuel. In order to improve the accuracy of control and enhance the matching between fuel injection control amount and fuel filling amount, an aircraft tank refueling vehicle fuel injection controller is composed of a fuel actuator composite controller based on disturbance observer (DOB) and a dual closed-loop controller. The calculated aircraft fuel filling amount is used as input to achieve intelligent fuel injection control of the aircraft tank refueling vehicle through the fuel injection controller. The test results show that the fuel injection control amount of the design method matches the aircraft fuel injection amount very well, almost completely overlapping. The fuel injection control speed curve is stable with minimal fluctuations. The pressure curve of the fuel pipeline system fluctuates to some extent in the initial stage, and then it hardly fluctuates again. The test results indicate that the overall fuel injection control accuracy of the design method is good.