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Cyber-Physical Systems Virtual Organization
Read-only archive of site from September 29, 2023.
CPS-VO
aircraft engine
biblio
Dynamic Threshold Design Based on Kalman Filter in Multiple Fault Diagnosis
Submitted by aekwall on Mon, 05/18/2020 - 10:48am
aircraft engine
uncertain systems
time domain response range calculation formula
state space equation
sensitivity requirements
Kalman filter
isolation systems
dynamic threshold range changes
dynamic threshold design
dynamic threshold algorithm
dynamic threshold
diagnosis system
current methods
constant threshold
bounded norm uncertainty
aircraft engine fault detection
Resiliency
aerospace engines
multiple fault diagnosis
fault diagnosis
Eigenvalues and eigenfunctions
Kalman filters
Time factors
Human Factors
Engines
cyber physical systems
uncertainty
Mathematical model
Robustness
robust control
Metrics
pubcrawl
