Integrated Engine Prognostics and Health Management (IEPHM) - PowerPoint PPT Presentation

1 / 6
About This Presentation
Title:

Integrated Engine Prognostics and Health Management (IEPHM)

Description:

Integrated Engine Prognostics and Health Management (IEPHM) Demonstrate an Integrated Set of PHM Technologies for Gas Path Health Determination – PowerPoint PPT presentation

Number of Views:62
Avg rating:3.0/5.0
Slides: 7
Provided by: jimwh6
Category:

less

Transcript and Presenter's Notes

Title: Integrated Engine Prognostics and Health Management (IEPHM)


1
Integrated Engine Prognostics and Health
Management (IEPHM)
Demonstrate an Integrated Set of PHM Technologies
for Gas Path Health Determination
2
Kalman Filter Theory
  • The current optimizer algorithm used in the
    tracking filter is a modified Kalman filter,
    based on feedback control. At each time step the
    sensor residuals are multiplied by the average
    gains matrix to adjust the QLTYs.
  • The Kalman filter is a recursive filter it
    estimates a process by using a form of feedback
    control. In theory, the Kalman filter can be
    optimal. The Kalman filter applied to the F414 is
    a linear approximation. For each iteration, it
    cycles through 2 sets of equations time update
    and measurement update.

3
Kalman Filter Algorithm Equations
Time Update Equations Measurement Update
Equations
4
Kalman Filter Applied to F414 Engine
  • X represents the QLTY estimates vector (8x1).
  • Notation notes the carrot over the X symbolizes
    that it is an estimate. The super minus
    represents the a priori estimate, while the X
    calculated in the measurement update equations
    represents the measurement corrected estimate.
  • Z is the sensor measurements vector (9x1). H is
    the average gains matrix (9x8) it remains
    constant.
  • P is the estimate error covariance (8x8) matrix.
  • K represents the Kalman gain (8x9) matrix.

5
Results
  • Certain assumptions were made to simply the
    Kalman filter for easier implementation on the
    F414.
  • For the linear stochastic difference equation
    (equation 1 of the time update equations)
  • A is an identity matrix. i.e. QLTYs arent
    dynamic.
  • There is no control input, so u is zero
  • Process noise, w, is white
  • Note In the real world, both w and u would be
    non-zero. However, because input data is coming
    from CLM_ENG into CLM_MOD, w is treated to be
    zero.
  • For the error covariance matrices
  • R (9x9), measurement error covariance and
  • Q (8x8), process error covariance, are constant
    diagonal matrices

6
Results
  • QLTY values were initially set to .001.
  • A nominal run at 17.5K ft and M.625 for 1080
    seconds was made.
  • The following figure compare the performance of
    the Kalman filter to the current tracking filter.
    The tracking filter out-performs the Kalman
    filter, obtaining a value as low as 10-5,
    while the Kalman filters minimum value was 10-4.

BLACK TF GREEN KALMAN
Write a Comment
User Comments (0)
About PowerShow.com