Design of Hybrid Deployment Architecture for Aircraft Software for Intelligent Applications

With the rapid development of intelligent applications, the mission execution mode of aircraft has gradually expanded from a single real-time control mode to a hybrid mode of real-time system and non-real-time system, which brings new challenges to the software deployment architecture of aircraft. The centralized architecture relies on the processing power of local hardware, and it is difficult to support the operation of complex intelligent algorithms, while the distributed architecture is affected by the communication delay and data synchronization uncertainty, and it is also difficult to meet the complex application scenarios of aircraft. On the basis of summarizing the development trend of aircraft technology, this study analyzed the requirements of real-time and non-real-time software architecture systems brought about by intelligent applications of aircraft, and designed a hybrid deployment architecture based on autonomous systems OpenEuler and UniProton, and then verified the performance of autonomous systems under the hybrid deployment architecture through deployment tests. The results show that the hybrid deployment architecture proposed in this scheme has a good applicability to the intelligent application of aircraft.