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
Link To Document :
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