DocumentCode
2012944
Title
A New Kind of Satellite Integrated Attitude Determination System
Author
Zhi-sheng, Wang ; Yuan-Sheng, Wu ; Huang-Zhong, Pu
Author_Institution
Nanjing Univ. of Aeronaut. & Astronaut., Nanjing
fYear
2007
fDate
May 30 2007-June 1 2007
Firstpage
3254
Lastpage
3258
Abstract
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 filtering can only guarantee global optimum.
Keywords
artificial satellites; attitude measurement; navigation; extended federated filtering algorithm; information allocation theorem; information conversation principle; information fusion; integrated navigation system; satellite integrated attitude determination system; Automatic control; Automation; Control systems; Filtering algorithms; Information filtering; Information filters; Loss measurement; Position measurement; Satellites; State estimation; attitude determination; extended federal filter; information allocation; information fusion; integrated navigation system;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Automation, 2007. ICCA 2007. IEEE International Conference on
Conference_Location
Guangzhou
Print_ISBN
978-1-4244-0817-7
Electronic_ISBN
978-1-4244-0818-4
Type
conf
DOI
10.1109/ICCA.2007.4376964
Filename
4376964
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