Solar-GPS Navigation Dataware System for Spacecraft

Alexander I. Tkachenko

doi:10.1615/JAutomatInfScien.v33.i11.30

Journal of Automation and Information Sciences

Editor-in-Chief: Arkadiy A. Chikriy (open in a new tab)

Associate Editors: Vyacheslav F. Gubarev (open in a new tab) Yuriy P. Kondratenko (open in a new tab) Nonna V. Turovyerova (open in a new tab)

Published 12 issues per year

ISSN Print: 1064-2315

ISSN Online: 2163-9337

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Solar-GPS Navigation Dataware System for Spacecraft

Volume 33, Issue 11, 2001, 12 pages

DOI: 10.1615/JAutomatInfScien.v33.i11.30

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Alexander I. Tkachenko
International Research and Training Center of Information Technologies and Systems of National Academy of Sciences of Ukraine and Ministry of Education and Science of Ukraine, Kyiv

ABSTRACT

The possibility of parameters determination of a spacecraft orbital motion and of parameters of motion about its mass-center using sun sensors and GPS (Global Positioning System) user equipment is considered. The problem of determination of above-mentioned parameters under essential uncertainty of initial conditions is solved by means of state estimation algorithm, that possesses considerable convergence properties.

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