TitleThe integration of the inertial, satellite and astroinformation in the problem of the navigation system correction
OrganizationInstitute of Automation and Control Processes Far Eastern Branch of the Russian Academy of Sciences (IACP FEB RAS)
AbstractWithin the framework of inertial navigating system correction problem the models of inertial, satellite and astroinformation integration are offered and investigated. The results of numerical experiments characterizing computational stability and efficiency of the problem solution in conditions of the measurements limited accuracy are presented.
Keywordsinertial navigation, astro-system, gyroscope, newtonometer, inverse problem, navigation satellite system
For citing this articleChislov K.A. The integration of the inertial, satellite and astroinformation in the problem of the navigation system correction // The Research of the Science City, 2012, no. 2, pp. 50-53.
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