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Journal of Automation and Information Sciences
SJR: 0.275 SNIP: 0.59 CiteScore™: 0.8

ISSN Imprimir: 1064-2315
ISSN En Línea: 2163-9337

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Journal of Automation and Information Sciences

DOI: 10.1615/JAutomatInfScien.v43.i2.40
pages 39-54

Nonlinear State Estimator Using the Data on Moving Horizon and its Application in the Problem of Spacecraft Attitude

Vyacheslav F. Gubarev
Institute of Space Research National Academy of Sciences of Ukraine State Space Agency of Ukraine Kiev, Ukraine
Alexander N. Daryin
M.V. Lomonosov Moscow State University (Russia)
Ivan A. Lysyuchenko
Institute for Applied Systems Analysis of National Technical University of Ukraine "Kiev Polytechnic Institute", Kiev

SINOPSIS

The possibility in principle of estimating the Euler−Krylov angles and projections of the angular velocity of a spacecraft by approximate data of incomplete measurements on the basis of the moving horizon method and non-linear estimator is considered. By means of numerical simulation a number of important properties of the method, including its robustness and conditions for stability, are established.


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