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
Link To Document :
بازگشت