DocumentCode :
174783
Title :
A least squares approach to size effect in inertial navigation
Author :
Eilon, S.
Author_Institution :
TAMAM Div., Israel Aerosp. Ind. Ltd., Yehud, Israel
fYear :
2014
fDate :
5-8 May 2014
Firstpage :
721
Lastpage :
732
Abstract :
This paper deals with the size effect problem in high-end Inertial Navigation Systems (INS). A focus is given to velocity errors in the geographical frame, which endure even after dynamic angular conditions are terminated. A least squares (LS) approach is taken to derive an algorithm for size effect compensation. The suggested algorithm implementation is based on low computation rate and does not involve highsampled increments. A performance analysis of the algorithm is presented, both in simulation and in real-life systems´ tests.
Keywords :
inertial navigation; least squares approximations; INS; LS approach; dynamic angular conditions; geographical frame; high-end inertial navigation systems; least squares approach; low computation rate; performance analysis; real-life system tests; size effect compensation; velocity errors; Acceleration; Accelerometers; Algorithm design and analysis; Navigation; Rotation measurement; Sensitivity; Vectors; High-end Inertial Naviagation Systems; Least Squares; Size Effect;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Position, Location and Navigation Symposium - PLANS 2014, 2014 IEEE/ION
Conference_Location :
Monterey, CA
Print_ISBN :
978-1-4799-3319-8
Type :
conf
DOI :
10.1109/PLANS.2014.6851438
Filename :
6851438
Link To Document :
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