DocumentCode
3512457
Title
Combined complementary filter For inertial navigation system
Author
Filiashkin, M. ; Novik, M.
Author_Institution
Nat. Aviation Univ., Kiev, Ukraine
fYear
2012
fDate
9-12 Oct. 2012
Firstpage
59
Lastpage
62
Abstract
This paper presents analysis of the complementary algorithm for inertial navigation systems. Suboptimal algorithm for sensors data fusion of the navigation system is proposed. This method employs combined complementary filter approach and attitude error equation of the inertial navigation system. Simulation results are presented to demonstrate the performance of the proposed approach.
Keywords
Kalman filters; inertial navigation; nonlinear filters; sensor fusion; attitude error equation; complementary filter approach; inertial navigation system; sensor data fusion; Filtering; Global Positioning System; Inertial navigation; Noise; Tin; complementary filter; data fusion; inertial navigation system;
fLanguage
English
Publisher
ieee
Conference_Titel
Methods and Systems of Navigation and Motion Control (MSNMC), 2012 2nd International Conference
Conference_Location
Kiev
Print_ISBN
978-1-4673-2551-6
Type
conf
DOI
10.1109/MSNMC.2012.6475087
Filename
6475087
Link To Document