NAU Harvester System
Determination of rotation parameters of unstabilizd artificial earth satellite (AES), presented by model “diffuse cylinder”
Вісник астрономічної школи
View Archive Info| Field | Value | |
| Title |
Determination of rotation parameters of unstabilizd artificial earth satellite (AES), presented by model “diffuse cylinder”
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| Creator |
Kolesnik S.Ya.
Paltsev N.G. |
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| Date |
2009
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| Source |
Astronomical School’s Report, 2009, Volume 6, Issue 1, P. 93-97
2411-6602 |
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| Identifier |
http://astro.nau.edu.ua/papers/AstSR_2009_Vol_6_Iss_1_P_93.pdf
10.18372/2411-6602.06.1093 |
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| Language |
ru
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| Description |
The algorithm is presented for determination of rotation axis (pole) coordinates and sidereal rotation period of satellite, simulated by the diffuse cylinder precessing around vector of angular moment of impulse with constant nutation angle. The Lambert's law of light reflection is accepted. Simultaneously, dependence of light reflection coefficient versus phase angle also is determined. The model simulations confirm serviceability of this method. The algorithm is proposed for estimation of accuracy of pole coordinates founded by this method.
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| Publisher |
National Aviation University
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| Format |
application/pdf
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