TY - JOUR
T1 - Extended federated filtering algorithm and its application in satellite integrated attitude determination system
AU - Wang, Zhi Sheng
AU - Liu, Jian Ye
AU - Zhou, Jun
PY - 2004/9
Y1 - 2004/9
N2 - An Extended Federated Filtering (EFF) algorithm is developed which can be applied to integrated navigation system and integrated attitude determination system. According to both information fusion theories and information conversation principle, it is proposed that information allocation is the inverse process of information fusion in EFF algorithm. The information allocation theorem is given and proved, which lays a theoretical foundation for EFF. Taking a certain satellite integrated attitude determination system as an example, the realization of EFF is discussed in detail. The theoretical analysis and simulation results show that EFF algorithm is less computation than present federated filtering algorithm, and EFF can guarantee both local optimum and global optimum, while present federated filter can only guarantee global optimum.
AB - An Extended Federated Filtering (EFF) algorithm is developed which can be applied to integrated navigation system and integrated attitude determination system. According to both information fusion theories and information conversation principle, it is proposed that information allocation is the inverse process of information fusion in EFF algorithm. The information allocation theorem is given and proved, which lays a theoretical foundation for EFF. Taking a certain satellite integrated attitude determination system as an example, the realization of EFF is discussed in detail. The theoretical analysis and simulation results show that EFF algorithm is less computation than present federated filtering algorithm, and EFF can guarantee both local optimum and global optimum, while present federated filter can only guarantee global optimum.
KW - Attitude determination
KW - Extended federated filter
KW - Information allocation
KW - Information fusion
KW - Integrated navigation system
UR - http://www.scopus.com/inward/record.url?scp=11144229795&partnerID=8YFLogxK
M3 - 文章
AN - SCOPUS:11144229795
SN - 1000-1328
VL - 25
SP - 570
EP - 575
JO - Yuhang Xuebao/Journal of Astronautics
JF - Yuhang Xuebao/Journal of Astronautics
IS - 5
ER -