DETERMINATION OF POLE AND ROTATION PERIOD OF NOT STABILIZED ARTIFICIAL SATELLITE BY USE OF MODEL

DETERMINATION OF POLE AND ROTATION PERIOD OF NOT STABILIZED ARTIFICIAL SATELLITE BY USE OF MODEL

The algorithm of determination of orientation of rotation axis (pole) and rotation period of satellite, simulated by a cylinder, which is precessing around of vector of angular moment of pulse with constant nutation angle is offered. The Lambert's law of light reflection is accepted. Simultaneo...

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Main Authors: S. Ya. Kolesnik, A. V. Dobrovolsky, N. G. Paltsev
Format: Article
Language:English
Published: Odessa I. I. Mechnykov National University 2017-03-01
Series:Odessa Astronomical Publications
Online Access:http://oap.onu.edu.ua/article/view/93214
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spelling doaj-7bc9fefb41e249ec9a4c4b4de44beb092020-11-25T02:32:48ZengOdessa I. I. Mechnykov National UniversityOdessa Astronomical Publications1810-42152017-03-01170333510.18524/1810-4215.2004.17.9321493214DETERMINATION OF POLE AND ROTATION PERIOD OF NOT STABILIZED ARTIFICIAL SATELLITE BY USE OF MODELS. Ya. Kolesnik0A. V. DobrovolskyN. G. PaltsevDepartment of Astronomy, Odessa State University T.G.Shevchenko Park, Odessa 65014 UkraineThe algorithm of determination of orientation of rotation axis (pole) and rotation period of satellite, simulated by a cylinder, which is precessing around of vector of angular moment of pulse with constant nutation angle is offered. The Lambert's law of light reflection is accepted. Simultaneously, dependence of light reflection coefficient versus phase angle is determined. The model's simulation confirm applicability of this method. Results of the calculations for artificial satellite No 28506 are carried out.http://oap.onu.edu.ua/article/view/93214
collection DOAJ
language English
format Article
sources DOAJ
author S. Ya. Kolesnik
A. V. Dobrovolsky
N. G. Paltsev
spellingShingle S. Ya. Kolesnik
A. V. Dobrovolsky
N. G. Paltsev
DETERMINATION OF POLE AND ROTATION PERIOD OF NOT STABILIZED ARTIFICIAL SATELLITE BY USE OF MODEL
Odessa Astronomical Publications
author_facet S. Ya. Kolesnik
A. V. Dobrovolsky
N. G. Paltsev
author_sort S. Ya. Kolesnik
title DETERMINATION OF POLE AND ROTATION PERIOD OF NOT STABILIZED ARTIFICIAL SATELLITE BY USE OF MODEL
title_short DETERMINATION OF POLE AND ROTATION PERIOD OF NOT STABILIZED ARTIFICIAL SATELLITE BY USE OF MODEL
title_full DETERMINATION OF POLE AND ROTATION PERIOD OF NOT STABILIZED ARTIFICIAL SATELLITE BY USE OF MODEL
title_fullStr DETERMINATION OF POLE AND ROTATION PERIOD OF NOT STABILIZED ARTIFICIAL SATELLITE BY USE OF MODEL
title_full_unstemmed DETERMINATION OF POLE AND ROTATION PERIOD OF NOT STABILIZED ARTIFICIAL SATELLITE BY USE OF MODEL
title_sort determination of pole and rotation period of not stabilized artificial satellite by use of model
publisher Odessa I. I. Mechnykov National University
series Odessa Astronomical Publications
issn 1810-4215
publishDate 2017-03-01
description The algorithm of determination of orientation of rotation axis (pole) and rotation period of satellite, simulated by a cylinder, which is precessing around of vector of angular moment of pulse with constant nutation angle is offered. The Lambert's law of light reflection is accepted. Simultaneously, dependence of light reflection coefficient versus phase angle is determined. The model's simulation confirm applicability of this method. Results of the calculations for artificial satellite No 28506 are carried out.
url http://oap.onu.edu.ua/article/view/93214
work_keys_str_mv AT syakolesnik determinationofpoleandrotationperiodofnotstabilizedartificialsatellitebyuseofmodel
AT avdobrovolsky determinationofpoleandrotationperiodofnotstabilizedartificialsatellitebyuseofmodel
AT ngpaltsev determinationofpoleandrotationperiodofnotstabilizedartificialsatellitebyuseofmodel
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