DocumentCode
324879
Title
Enhanced precision attitude determination algorithms
Author
Lam, Quang M. ; Wu, Andy
Author_Institution
Intelligent Syst. Technol., Fairfax, VA, USA
Volume
1
fYear
1998
fDate
21-28 Mar 1998
Firstpage
61
Abstract
In this paper, a robust filtering scheme is developed to enhance the performance of the attitude determination system (ADS). The filter structure is constructed based on extended Kalman filtering (EKF) scheme to accommodate for nonlinear measurement process; however, the overall filtering scheme is augmented with two additional mechanisms to provide appropriate treatments to the nonwhiteness and nonstationary signals arising from the ADS sensor package. These two mechanisms are nonwhite noise identifier and white noise covariance updater for the EKF process noise and measurement noise matrices. The first mechanism is aimed to address the nonwhiteness and nonstationary ADS noises by reconstructing them for cancellation at the measurement level while the second mechanism is intended to fine-tune the performance of the EKF, thereby providing the EKF with an operational condition to produce enhanced precision attitude determination performance
Keywords
Kalman filters; attitude control; robust control; space vehicles; attitude determination algorithms; extended Kalman filtering; measurement noise matrices; nonlinear measurement process; nonstationary signals; nonwhiteness signals; process noise; robust filtering scheme; sensor package; white noise covariance updater; Covariance matrix; Filtering; Kalman filters; Noise cancellation; Noise measurement; Packaging; Position measurement; Robustness; Signal processing; White noise;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 1998 IEEE
Conference_Location
Snowmass at Aspen, CO
ISSN
1095-323X
Print_ISBN
0-7803-4311-5
Type
conf
DOI
10.1109/AERO.1998.686673
Filename
686673
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