Abstract

For different application scenarios, aerospace vehicle control systems may use different flight control hardware platforms, flight control strategies, and control functions, and the variability in adoption may lead to difficulties in the development and transplantation of software for general purpose. In this paper, we propose a new idea to adopt modular design to decompose the vehicle control software functions into sensor data unpacking, navigation calculation, attitude control calculation, data fusion, control output, hardware driver, thread scheduling and other modules, modular packaging design or each function, and hierarchical design for the overall architecture to achieve the minimum modification to meet the development needs of different application scenarios. The overall architecture is designed in a hierarchical way to meet the development needs of different applications with minimal modifications and good scalability.

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