运载火箭测量系统综合化设计与实现OACSTPCD

In allusion to the problems of single function,fixed working system,and closed system architecture of traditional measurement systems for launch vehicles,a suitable open system architecture based on integrated modular avionics(IMA)for current applications is proposed based on the constraints of the launch vehicle platform and by analysing the technical characteristics,iterative process,and limitations of the system.The development of the comprehensive RF terminal based on this architecture is completed,achieving a miniaturized,lightweight,low-power,and flexible and scalable comprehensive measurement system.The designed system can meet the overall application requirements and has broad application prospects in the aerospace field.