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Kalman Filter Constraint Tuning for Turbofan Engine Health Estimation

AUTHOR Administration (Nasa), National Aeronaut
PUBLISHER Independently Published (08/05/2020)
PRODUCT TYPE Paperback (Paperback)

Description
Kalman filters are often used to estimate the state variables of a dynamic system. However, in the application of Kalman filters some known signal information is often either ignored or dealt with heuristically. For instance, state variable constraints are often neglected because they do not fit easily into the structure of the Kalman filter. Recently published work has shown a new method for incorporating state variable inequality constraints in the Kalman filter, which has been shown to generally improve the filter s estimation accuracy. However, the incorporation of inequality constraints poses some risk to the estimation accuracy as the Kalman filter is theoretically optimal. This paper proposes a way to tune the filter constraints so that the state estimates follow the unconstrained (theoretically optimal) filter when the confidence in the unconstrained filter is high. When confidence in the unconstrained filter is not so high, then we use our heuristic knowledge to constrain the state estimates. The confidence measure is based on the agreement of measurement residuals with their theoretical values. The algorithm is demonstrated on a linearized simulation of a turbofan engine to estimate engine health. Simon, Dan and Simon, Donald L. Glenn Research Center NASA/TM-2005-213962, ARL-MR-621, E-15278 TURBOFAN ENGINES; KALMAN FILTERS; ESTIMATES; HEURISTIC METHODS; RISK; SIMULATION; INEQUALITIES
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ISBN-13: 9798672766317
Binding: Paperback or Softback (Trade Paperback (Us))
Content Language: English
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Page Count: 36
Carton Quantity: 113
Product Dimensions: 8.50 x 0.07 x 11.02 inches
Weight: 0.24 pound(s)
Country of Origin: US
Subject Information
BISAC Categories
Reference | Research
Reference | Space Science - General
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Kalman filters are often used to estimate the state variables of a dynamic system. However, in the application of Kalman filters some known signal information is often either ignored or dealt with heuristically. For instance, state variable constraints are often neglected because they do not fit easily into the structure of the Kalman filter. Recently published work has shown a new method for incorporating state variable inequality constraints in the Kalman filter, which has been shown to generally improve the filter s estimation accuracy. However, the incorporation of inequality constraints poses some risk to the estimation accuracy as the Kalman filter is theoretically optimal. This paper proposes a way to tune the filter constraints so that the state estimates follow the unconstrained (theoretically optimal) filter when the confidence in the unconstrained filter is high. When confidence in the unconstrained filter is not so high, then we use our heuristic knowledge to constrain the state estimates. The confidence measure is based on the agreement of measurement residuals with their theoretical values. The algorithm is demonstrated on a linearized simulation of a turbofan engine to estimate engine health. Simon, Dan and Simon, Donald L. Glenn Research Center NASA/TM-2005-213962, ARL-MR-621, E-15278 TURBOFAN ENGINES; KALMAN FILTERS; ESTIMATES; HEURISTIC METHODS; RISK; SIMULATION; INEQUALITIES
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Paperback