DocumentCode :
1410869
Title :
Hierarchical adaptive Kalman filtering for interplanetary orbit determination
Author :
Chaer, Wassim S. ; Bishop, Robert H. ; Ghosh, Joydeep
Author_Institution :
SDT Res. Group, Ft. Worth, TX, USA
Volume :
34
Issue :
3
fYear :
1998
fDate :
7/1/1998 12:00:00 AM
Firstpage :
883
Lastpage :
896
Abstract :
A modular and flexible approach to adaptive Kalman filtering has recently been introduced using the framework of a mixture-of-experts regulated by a gating network. Each expert is a Kalman filter modeled with a different realization of the unknown system parameters. The unknown or uncertain parameters can include elements of the state transition matrix, observation mapping matrix, process noise covariance matrix, and measurement noise covariance matrix. The gating network performs on-line adaptation of the weights given to individual filters based on performance. The mixture-of-experts approach is extended here to a hierarchical architecture which involves multiple levels of gating. The proposed architecture provides a multilevel hypothesis testing capability. The utility of the hierarchical architecture is illustrated via the problem of interplanetary navigation (Mars Pathfinder) using simulated radiometric data. It serves as a useful tool for assisting navigation teams in the process of selecting the parameters of the navigational filter over various operating regimes. It is shown that the scheme has the capability of detecting changes in the system parameters and switching filters appropriately for optimal performance. Furthermore, the expectation-maximization (EM) algorithm is shown to be applicable in the proposed framework
Keywords :
adaptive Kalman filters; iterative methods; learning (artificial intelligence); maximum likelihood estimation; navigation; neural net architecture; realisation theory; state estimation; tracking filters; Mars Pathfinder; expectation-maximization algorithm; gating network; hierarchical adaptive Kalman filtering; interplanetary navigation; interplanetary orbit determination; iterative MAXLE; learning algorithm; measurement noise covariance matrix; mixture-of-experts; modular flexible approach; multilevel hypothesis testing capability; multiple levels of gating; navigational filter; neuron cells; observation mapping matrix; on-line adaptation; optimal performance; process noise covariance matrix; simulated radiometric data; spacecraft tracking; state estimation; state transition matrix; unknown system parameters; Adaptive filters; Covariance matrix; Extraterrestrial measurements; Filtering; Kalman filters; Mars; Noise measurement; Radio navigation; Radiometry; Testing;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/7.705895
Filename :
705895
Link To Document :
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