TY - GEN
T1 - High precision and convenient extension simulation platform for satellite attitude and orbit system
AU - Cui, Hongzheng
AU - Han, Chao
AU - Chen, Pei
AU - Luo, Qinqin
PY - 2012
Y1 - 2012
N2 - 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.
AB - 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.
KW - Satellite attitude and orbit
KW - convenient extension
KW - high precision
KW - inheritability
KW - simulation platform
UR - https://www.scopus.com/pages/publications/84863420656
U2 - 10.1117/12.920918
DO - 10.1117/12.920918
M3 - 会议稿件
AN - SCOPUS:84863420656
SN - 9780819490254
T3 - Proceedings of SPIE - The International Society for Optical Engineering
BT - Fourth International Conference on Machine Vision, ICMV 2011
T2 - 4th International Conference on Machine Vision: Machine Vision, Image Processing, and Pattern Analysis, ICMV 2011
Y2 - 9 December 2011 through 10 December 2011
ER -