DocumentCode
391347
Title
Optimal filtering in the presence of faulty measurement biases
Author
Rapoport, Ilia ; Oshman, Yaakov
Author_Institution
Dept. of Aerosp. Eng., Technion-Israel Inst. of Technol., Haifa, Israel
Volume
2
fYear
2002
fDate
10-13 Dec. 2002
Firstpage
2236
Abstract
The problem of fault tolerant estimation with application to a system subjected to faulty measurement biases is addressed. A new estimation approach, called fault adaptive filtering, is proposed. The proposed estimation scheme consists of a single minimum variance state estimator, which takes into account fault probabilities, combined with a fault estimator, which provides estimates of these probabilities. Unlike the multiple model approach this method does not require a large number of parallel filters. On the other hand, unlike separate estimation and fault detection techniques, the fault adaptive filter is able to utilize partial information about the existence of faults. A numerical example of spacecraft attitude determination is presented, which demonstrates the performance of the proposed approach.
Keywords
aerospace control; aircraft navigation; fault tolerance; parameter estimation; aerospace navigation; fault adaptive filter; fault adaptive filtering; fault detection; fault estimator; fault tolerant estimation; optimal filtering; spacecraft attitude determination; Adaptive filters; Fault detection; Fault tolerant systems; Filtering; Missiles; Navigation; Position measurement; Probability; Space vehicles; State estimation;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 2002, Proceedings of the 41st IEEE Conference on
ISSN
0191-2216
Print_ISBN
0-7803-7516-5
Type
conf
DOI
10.1109/CDC.2002.1184864
Filename
1184864
Link To Document