中圖分類號：TP23 文獻標志碼：A DOI: 10.16157/j.issn.0258-7998.233823 中文引用格式： 楊德輝，周淦，李林峰. 基于領(lǐng)域驅(qū)動的測控任務(wù)評定系統(tǒng)設(shè)計與實現(xiàn)[J]. 電子技術(shù)應(yīng)用，2023，49(9)：138-144. 英文引用格式： Yang Dehui，Zhou Gan，Li Linfeng. Design and implementation of measurement and control task evaluation system based on domain-driven[J]. Application of Electronic Technique，2023，49(9)：138-144.
Design and implementation of measurement and control task evaluation system based on domain-driven
Yang Dehui，Zhou Gan，Li Linfeng
(National Computer System Engineering Research Institute of China， Beijing 100083， China)
Abstract： With the continuous progress of aerospace technology, especially the rapid development of commercial aerospace in recent years, high-density space launch has become the norm. As one of the important business systems of the space launch site, the operational ability and efficiency of the system will greatly affect the results of the implementation of the space launch mission. Therefore, it is necessary to carry out the research on the decision-making and evaluation of the process of the measurement and control mission. Considering that the rapid assessment of future measurement and control tasks will present the trend of less people, generalization, automation and intelligence. This paper presents a design idea of measurement and control task evaluation system based on domain driven design. Through in-depth analysis of measurement and control task evaluation business, combined with the characteristics of domain-driven design and micro-service architecture, the whole system is designed through domain model design, micro-service identification, micro-service implementation and other steps. Finally, the feasibility of this scheme is verified by combining with typical space launch TT&C mission scenarios, which provides reference and ideas for further improving the efficiency of TT&C mission evaluation in China.
Key words : commercial aerospace；measurement and control tasks；domain driven design；micro service；evaluation system
