DocumentCode
2835421
Title
Method based on H _ 8 Filter and Kalman Filter for Gravity Anomaly Distortion Correction
Author
Liye, Zhao ; Hongsheng, Li ; Bailing, Zhou ; Kunyu, Li
Author_Institution
Sch. of Instrum. Sci. & Eng., Southeast Univ., nanjing
fYear
2008
fDate
Aug. 29 2008-Sept. 2 2008
Firstpage
879
Lastpage
883
Abstract
Based on the strong robust performance of filter for the uncertainty of the system model and noises, a new method based on filter and Kalman inverse filter for gravity anomaly distortion correction is proposed to ameliorate the performance of single inverse Kalman filter. This method deduces the system state equation according to the transfer function of actual gravimeter system firstly, then filter is used to inhibit the influence of the measurement noises, finally inverse Kalman filter is adapted and the corrected gravity anomaly signal is obtained. Simulations using actual measurement data proved that the decay introduced by measurement noises of gravity anomaly correction procedure had been effectively inhibit and the precision of system had been improved apparently.
Keywords
Kalman filters; H _ infin filter; Kalman filter; gravity anomaly distortion correction; system state equation; Distortion measurement; Equations; Gravity; Inertial navigation; Information filtering; Information filters; Kalman filters; Noise measurement; Predistortion; Time measurement; Kalman inverse filter; distortion correction; filter; gravimeter; gravity anomaly;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Science and Information Technology, 2008. ICCSIT '08. International Conference on
Conference_Location
Singapore
Print_ISBN
978-0-7695-3308-7
Type
conf
DOI
10.1109/ICCSIT.2008.149
Filename
4624993
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