DocumentCode
1162946
Title
A Crame´r-Rao-type estimation lower bound for systems with measurement faults
Author
Rapoport, Ilia ; Oshman, Yaakov
Author_Institution
Dept. of Aerosp. Eng, Technion Israel Inst. of Technol., Haifa, Israel
Volume
50
Issue
9
fYear
2005
Firstpage
1234
Lastpage
1245
Abstract
A Crame´r-Rao-type lower bound is presented for systems with measurements prone to discretely-distributed faults, which are a class of hybrid systems. Lower bounds for both the state and the Markovian interruption variables (fault indicators) of the system are derived, using the recently presented sequential version of the Crame´r-Rao lower bound (CRLB) for general nonlinear systems. Because of the hybrid nature of the systems addressed, the CRLB cannot be directly applied due to violation of its associated regularity conditions. To facilitate the calculation of the lower bound, the hybrid system is first approximated by a system in which the discrete distribution of the fault indicators is replaced by an approximating continuous one. The lower bound is then obtained via a limiting process applied to the approximating system. The results presented herein facilitate a relatively simple calculation of a nontrivial lower bound for the state vector of systems with fault-prone measurements. The CRLB-type lower bound for the interruption process variables turns out to be trivially zero, however, a nontrivial, non-CRLB-type bound for these variables has been recently presented elsewhere by the authors. The utility and applicability of the proposed lower bound are demonstrated via a numerical example involving a simple global positioning system (GPS)-aided navigation system, where the GPS measurements are fault-prone due to their sensitivity to multipath errors.
Keywords
Markov processes; approximation theory; estimation theory; fault diagnosis; nonlinear systems; parameter estimation; state estimation; vectors; Cramer-Rao-type lower bound; GPS aided navigation system; GPS measurements; Markovian interruption variables; approximating system; estimation error lower bound; fault detection; fault indicators; general nonlinear systems; global positioning system; hybrid systems; measurement fault; multipath errors; Acceleration; Colored noise; Control systems; Global Positioning System; Magnetic field measurement; Magnetic sensors; Navigation; Nonlinear systems; Space vehicles; Stability; Estimation error lower bound; fault detection and isolation; hybrid systems;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/TAC.2005.854579
Filename
1506933
Link To Document