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
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;
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
DOI :
10.1109/MSNMC.2012.6475074
