Determination of Nanosatellite Attitude in the Regime of Noncontrolled Motion

Alexander I. Tkachenko

doi:10.1615/J Automat Inf Scien.v37.i8.60

Journal of Automation and Information Sciences

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

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

Publicou 12 edições por ano

ISSN Imprimir: 1064-2315

ISSN On-line: 2163-9337

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Determination of Nanosatellite Attitude in the Regime of Noncontrolled Motion

Volume 37, Edição 8, 2005, pp. 58-68

DOI: 10.1615/J Automat Inf Scien.v37.i8.60

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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

RESUMO

The problem of determining attitude of a small spacecraft under conditions, when limitations of energy resources, mass and size of the object force one to refuse controlling its motion with respect to the mass-center. The suggested solution is based on readings of the on-board magnetometer and the familiar from literature means of imitation of solar sensor by comparison of values of electric potential checked on the elements of solar batteries panels.

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