Structure Design and Generation of Bookbinding parameters for Launch Vehicle Flight Software

In the design process of large launch vehicle, task diversity, complexity and economy are becoming more and more challenging. With the use of the launch vehicle-borne computer, the flight software can realize the variable parameter design of the system, and decoupling between the mission and the software, generalized design can be configured by configuring the design and using parameters, to meet the diversified mission requirements of the spacecraft in the future.