DocumentCode
3512147
Title
Perspectives of integrated inertial-satellite systems development of civil aviation aircraft
Author
Sineglazov, V.M. ; Zaharin, F.M.
Author_Institution
Nat. Aviation Univ., Kiev, Ukraine
fYear
2012
fDate
9-12 Oct. 2012
Firstpage
9
Lastpage
12
Abstract
Using an inertial navigation system and Global Positioning System together is preferable to using any of them separately. Derived benefits depend on the level of combining information. Inertial navigation systems/ Global Positioning System integration architectures are defined as separate, loosely and tightly coupled, deeply integrated configurations.
Keywords
Global Positioning System; aircraft; inertial navigation; Global Positioning System integration architecture; civil aviation aircraft; inertial navigation system; integrated inertial-satellite system development; Accuracy; Computers; Couplings; Global Positioning System; Reliability; Resistance; Silicon compounds; Global Positioning System; aircraft; inertial navigation systems; integration;
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.2012.6475074
Filename
6475074
Link To Document