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Journal of Automation and Information Sciences

Publicado 12 números por año

ISSN Imprimir: 1064-2315

ISSN En Línea: 2163-9337

SJR: 0.173 SNIP: 0.588 CiteScore™:: 2

Indexed in

Determination of Nanosatellite Attitude in the Regime of Noncontrolled Motion

Volumen 37, Edición 8, 2005, pp. 58-68
DOI: 10.1615/J Automat Inf Scien.v37.i8.60
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SINOPSIS

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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