The Design and Implementation of Spacecraft Co-simulation Platform

被引:0
作者
Yin, Hang [1 ]
Gao, Yong Ming [1 ]
Wang, Chao [1 ]
Li, Xin Xing [2 ]
机构
[1] Acad Equipment Beijing, Beijing 101416, Peoples R China
[2] China Maritime Satellite Tracking & Control Dept, Shanghai, Peoples R China
来源
MANUFACTURING ENGINEERING AND AUTOMATION II, PTS 1-3 | 2012年 / 591-593卷
关键词
Co-Simulation; ADAMS; HLA; RTI; Spacecraft; Platform; IDENTIFICATION;
D O I
10.4028/www.scientific.net/AMR.591-593.174
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
With the continuous improvement of complexity in the space simulation system and the enhancement of multi-technology integration, the co-simulation technology is an important way to solve complex simulation problems in the big system. After analysis of relative theories and main methods of co-simulation, collaboration data interfaces among multiple software are improved and matched with a number of simulation software system. The co-simulation framework is designed and a set of spacecraft dynamics co-simulation analysis system is established on the frame of HLA/RTI and on the principle of co-simulation technology. The key task on orbit service of the spacecraft is modeled and simulated. The software can complete the work that a single simulation software could not be done and achieve good results.
引用
收藏
页码:174 / +
页数:2
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