Title :
Federated Adaptive Kalman Filtering and its application
Author_Institution :
Sch. of Autom. Sci. & Electr. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing
Abstract :
In order to deal with the problem in which the Federated Kalman Filtering (FKF) may be instable or divergent when noise statistics is unknown, a new federated filtering is presented, which is defined as Federated Adaptive Kalman Filtering (FAKF). A factor of modified the measurement noise covariance was built by using the ratio between filter residual and actual residual in FAKF. The adaptive estimation of FKF was realized by online modifying the measurement noise covariance. FAKF and FKF were compared using practical measuring data in inertial navigation system/global positioning system/double-star system (INS/GPS/DS) integrated navigation system. Simulation results show that FAKF has adaptability and has better estimation accuracy than the FKF when noise statistics information is unknown.
Keywords :
Global Positioning System; adaptive Kalman filters; inertial navigation; statistical analysis; double-star system; federated adaptive Kalman filtering; global positioning system; inertial navigation system; integrated navigation system; measurement noise covariance; noise statistics information; Adaptive estimation; Adaptive filters; Filtering; Global Positioning System; Inertial navigation; Kalman filters; Noise measurement; Position measurement; Signal to noise ratio; Statistics; adaptive filtering; federated filtering; integrated navigation system; satellite positioning system;
Conference_Titel :
Intelligent Control and Automation, 2008. WCICA 2008. 7th World Congress on
Conference_Location :
Chongqing
Print_ISBN :
978-1-4244-2113-8
Electronic_ISBN :
978-1-4244-2114-5
DOI :
10.1109/WCICA.2008.4593122