DocumentCode
670320
Title
Prediction of inertial navigation system error dynamics in INS/GPS system
Author
Filyashkin, N.K. ; Yatskivsky, V.S.
Author_Institution
Aviation Comput.-Integrated Complexes Dept., Nat. Aviation Univ., Kiev, Ukraine
fYear
2013
fDate
15-17 Oct. 2013
Firstpage
206
Lastpage
209
Abstract
This paper discusses methods of improving precision characteristics of an inertial navigation system in integrated Inertial Navigation System / Global Positioning System by prediction of evolution of inertial navigation system errors. The results of mathematical modeling, which confirm the feasibility of this approach for improving accuracy of inertial navigation system in offline mode, are given.
Keywords
Global Positioning System; inertial navigation; Global Positioning System; INS-GPS system; error dynamics; integrated inertial navigation system; Global Positioning System; Inertial navigation; Integrated circuit modeling; Kalman filters; Mathematical model; Silicon compounds; Inertial Navigation System / Global Positioning System; error dynamics; error models; identification; system integration;
fLanguage
English
Publisher
ieee
Conference_Titel
Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD), 2013 IEEE 2nd International Conference
Conference_Location
Kiev
Print_ISBN
978-1-4799-3305-1
Type
conf
DOI
10.1109/APUAVD.2013.6705327
Filename
6705327
Link To Document