“…Consider the steady-state Kalman filter model of an LCR associated with different types of fault conditions denoted by subscript as (5) where is the Kalman filter model's state-space variables (displacement and speed of the shuttle), is the system matrix, is the input matrix, is the input vector, is the Kalman filter model's input noise matrix, is the input noise with zero mean and variance of (6) is the measurement vector (displacement and speed of the shuttle), is the output matrix, is the output measurement noise, independent from , with zero mean value as (7) Kalman filter model representation of a system is (8) where is the estimation of state space variable, is the actual output expected from the model, and is the Kalman filter gain recursively obtained through the following procedure: for (9) where is the covariance matrix updated by (10) The covariance matrix updates the Kalman gains recursively. The residual signal is defined as the difference between the output of the Kalman filter model and that of the actual operating system.…”