The errors of integrated inertial and satellite navigation system (ISNS) with correction scheme is investigated. The mathematical models describing the error of navigation parameters evaluation in the integrated system have been obtained. The model of integrated ISNS was compiled using a software package Simulink. As a result the diagrams of ISNS errors in dynamic mode of operation and accuracy analysis have been obtained.
navigation, integrated inertial-satellite navigation system
"Doslidzhennia pokhybok inertsialno-suputnykovoi navihatsiinoi systemy" ,
Science and Technology of the Air Force of Ukraine,