CAJ | 학술논문

为了进一步提高星载软件复用程度和解决航天器软件开发效率低下的问题，对星载软件特性和软件构件技术进行了分析和研究；对星载软件构件进行了定义，提出了一种基于非面向对象语言的、适用于星载软件开发和应用环境的星载软件构件模型。基于该模型开发的星载软件构件，具备独立性、完整性、可组装性和功能性。除此之外，对基于这种模型的星载软件构件设计、开发和使用方法进行了介绍，可以为采用非面向对象语言进行星载软件构件开发提供参考。在多个型号中对该技术展开实践，实践结果表明：提出的星载软件构件设计方法能够将星载软件开发效率提高2～5倍。
위료진일보제고성재연건복용정도화해결항천기연건개발효솔저하적문제，대성재연건특성화연건구건기술진행료분석화연구；대성재연건구건진행료정의，제출료일충기우비면향대상어언적、괄용우성재연건개발화응용배경적성재연건구건모형。기우해모형개발적성재연건구건，구비독립성、완정성、가조장성화공능성。제차지외，대기우저충모형적성재연건구건설계、개발화사용방법진행료개소，가이위채용비면향대상어언진행성재연건구건개발제공삼고。재다개형호중대해기술전개실천，실천결과표명：제출적성재연건구건설계방법능구장성재연건개발효솔제고2～5배。
In order to further improve the reusability of the on‐board software and to solve the problem of the on‐board software inefficient development , the characteristics of the spacecraft software and the software component technology were analyzed . Then a definition of the on‐board software component was given , and an on‐board software component model suitable for spacecraft was proposed based on the non‐object oriented language . The on‐board software components are independent ,integrate ,assemble and functional .Besides ,the method for the on‐board software component design ,develop and implement was described .It can be the guide of the on‐board software component development based on the non‐object oriented language .Some examples were given ,in which the software systems were developed according the proposed method . The results show that spacecraft software component development methods are effective , and the spacecraft software development efficiency can be increased by 200% ~500% .