Publication Date:
2016-06-07
Description:
A methodology for estimating initial mean and covariance parameters in a Kalman filter model from an ensemble of nonidentical tests is presented. In addition, the problem of estimating time constants and process noise levels is addressed. Practical problems such as developing and validating inertial instrument error models from laboratory test data or developing error models of individual phases of a test are generally considered.
Keywords:
ASTRODYNAMICS
Type:
NASA. Goddard Space Flight Center Fifth Ann. Flight Mech.(Estimation Theory Symp.; 29 p
Format:
application/pdf
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