航天器轨道设计系统的小型化实现

Realization of A Small System of Spacecraft Orbit Design

简要介绍了所开发的航天器轨道设计系统的功能,详细描述了这种小型轨道设计系统的实现策略、模块划分和总体结构。最后,指出了系统开发中的关键技术并概括了系统的性能。

This paper introduces the functions of the spacecraft orbit design system briefly, then describes the realization scheme, the modules and the structure of the small system detailedly. At last, it points out the kernel technology and summarizes the performance of the system.