High Precision and Convenient Extension Simulation Platform for Satellite Attitude and Orbit System

摘要：

In this paper, a high precision and convenient extension simulation platform for satellite attitude and orbit system is developed, to demonstrate the satellite attitude and orbit system for given space mission, and test the new underdeveloped algorithms for attitude/orbit dynamics, attitude determination, orbit navigation, and attitude/orbit control. The simulation platform is based on Matlab/Simulink software, using the technique of Simulink modeling, importing C/Fortran code in Matlab/Simulink, and embedded Matlab function, with beautiful reusability, inheritability and expansibility. The paper orderly presents the background behind the development of the platform, the platform design architecture and capability, the validity of the platform, the inheritability and expansibility of the platform, the platform implementation example for Chinese weather satellite (FY-3), and the future development for the platform.

关键词： satellite attitude and orbit simulation platform Inheritability high precision convenient extension

作者: Cui Hongzheng Han Chao Chen Pei Luo Qingqin

作者单位: School of Astronautics Beihang University, BUAA Beijing, P. R. China

会议类型: 国际会议

会议名称: 2010 International Conference on Software and Computing Technology(2010年软件与计算机技术国际会议 ICSCT 2010)

会议地点: 昆明

会议语种:英文

页码: 245-249

在线出版日期: 2010-10-17（万方平台首次上网日期，不代表论文的发表时间）