DocumentCode :
982285
Title :
Active Estimation for Jump Markov Linear Systems
Author :
Blackmore, Lars ; Rajamanoharan, Senthooran ; Williams, Brian C.
Author_Institution :
NASA Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
Volume :
53
Issue :
10
fYear :
2008
Firstpage :
2223
Lastpage :
2236
Abstract :
Jump Markov Linear Systems are convenient models for systems that exhibit both continuous dynamics and discrete mode changes. Estimating the hybrid discrete-continuous state of these systems is important for control and fault detection. Existing solutions for hybrid estimation approximate the belief state by maintaining a subset of the possible discrete mode sequences. This approximation can cause the estimator to lose track of the true mode sequence when the effects of discrete mode changes are subtle. In this paper, we present a method for active hybrid estimation, where control inputs can be designed to discriminate between possible mode sequences. By probing the system for the purposes of estimation, such a sequence of control inputs can greatly reduce the probability of losing the true mode sequence compared to a nominal control sequence. Furthermore, by using a constrained finite horizon optimization formulation, we are able to guarantee that a given control task is achieved, while optimally detecting the hybrid state. In order to achieve this, we present three main contributions. First, we develop a method by which a sequence of control inputs is designed in order to discriminate optimally between a finite number of linear dynamic system models. These control inputs minimize a novel, tractable upper bound on the probability of model selection error. Second, we extend this approach to develop an active estimation method for Jump Markov Linear Systems by relating the probability of model selection error to the probability of losing the true mode sequence. Finally, we make this method tractable using a principled pruning technique. Simulation results show that the new method applied to an aircraft fault detection problem significantly decreases the probability of a hybrid estimator losing the true mode sequence.
Keywords :
Markov processes; continuous time systems; discrete time systems; linear systems; active estimation; aircraft fault detection problem; continuous dynamics change; discrete mode change; discrete-continuous state; fault detection; jump Markov linear system; linear dynamic system model; nominal control sequence; principled pruning technique; probability; Aerodynamics; Biological system modeling; Control systems; Fault detection; Linear systems; NASA; Optimal control; Propulsion; Space technology; State estimation; Estimation; fault diagnosis; hybrid systems; switching systems;
fLanguage :
English
Journal_Title :
Automatic Control, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9286
Type :
jour
DOI :
10.1109/TAC.2008.2006100
Filename :
4668522
Link To Document :
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