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The uneven direct lift level of an aircraft can cause flight yaw issues. To achieve effective control of the aircraft's flight capability, an aircraft direct lift control system based on EMD and closed-loop testing is designed. In the FSEU architecture, the ARINC429 bus closed-loop mechanism is set up, combined with the servo control module and real-time onboard terminal, to achieve the establishment of the application mode of the aircraft direct lift control system. Define the conditions based on the hidden EMD information, solve the mass cardiac mechanics equation, and then calculate the specific value of heading deviation according to the principles of aerodynamic characteristics to complete the aircraft lift control based on EMD. Based on the memory network cross-linking environment, configure the model machine organization to improve the closed-loop testing function. The experimental results show that the application of the designed system can improve the problem of uneven direct lift levels, control the aircraft's flight yaw angle within the numerical range of 0 ° -20 °, and achieve effective control of the aircraft's flight capability.