Article

Cover

Title

The integration of the inertial, satellite and astroinformation in the problem of the navigation system correction

Author

K.A. Chislov

Organization

Institute of Automation and Control Processes Far Eastern Branch of the Russian Academy of Sciences (IACP FEB RAS)
Vladivostok, Russia

Abstract

Within 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.

Keywords

inertial navigation, astro-system, gyroscope, newtonometer, inverse problem, navigation satellite system

For citing this article

Chislov 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.

This Article is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License (CC BY-NC 4.0).