sch -2卫星多年观测的光度分析

Pub Date : 2023-04-28 DOI:10.15407/knit2023.02.086
V. Epishev, І.I. Motrunich, V. Perig, I. Neubauer, P. Guranich, A.I. Susla, M. Koshkin
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引用次数: 0

摘要

2011年8月17日,“第聂伯罗”号运载火箭从Yasny发射基地将“锡西-2”卫星送入地球轨道。乌克兰光学观测站立即开始记录卫星的光度曲线。在2012年中期,确定了Sich-2航天器有一定时期的自旋转并且可能已经失败。这一点后来得到了官方消息来源的证实。基于对地球上的sch -2人造卫星在乌日哥罗德和敖德萨的长期观测,研究了它从发射到2022年在轨道上的行为。通过对具有三自由度和复杂曲面设计特征的空间飞行器旋转动力学的研究,揭示了光度法与位置数据相结合的可能性。在文章中,作者确定了Sich-2航天器的自旋轴与其垂直轴重合,垂直轴围绕“卫星中心-地球中心”的方向进动。结果发现一对相对的psb相互垂直放置。卫星轨道周期的计算值为Porb = 99.5 min,岁差周期的平均值为Ppr ~ 90.5 sec,分析了ssi -2自旋周期的变化。在Po = 11.95…3.63…5.06秒范围内,以9年为周期变化。同时确定了同一时期的岁差周期在Рpr = 71.0…234.0…226.0秒范围内变化,旋转轴的岁差相对于卫星中心到地球中心的方向的夹角在38°…28°范围内。
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ANALYSIS OF PHOTOMETRY OF THE SICH-2 SATELLITE ON A MULTI-YEAR OBSERVATION INTERVALS
On August 17, 2011, a Dnipro vehicle launched the Sich-2 satellite into Earth’s orbit from the Yasny launch base. Ukrainian optical observation stations immediately began recording the satellite’s photometric light curves. In mid-2012, it was established that the Sich-2 spacecraft had a certain period of self-rotation and may have failed. This was confirmed later by official sources. Based on long-term observations of the Sich-2 artificial satellite of the Earth from Uzhgorod and Odesa, its behavior in orbit from the moment of launch until 2022 was investigated. The paper reveals the possibilities of the photometric method in combination with positional data from the research on the dynamics of the rotation of space vehicles with three degrees of freedom and complex design features of surfaces. In the article, the authors determined that the axis of self-rotation of the Sich-2 spacecraft coincides with its vertical axis, which precesses around the direction “the center of the satellite — the center of the Earth”. It was found that a pair of opposite PSBs are placed perpendicular to each other. The calculated value of the orbital period of the satellite was Porb = 99.5 min. and the average value of the precession period Ppr ~ 90.5 sec. The change in the period of selfrotation of the Sich-2 spacecraft was analyzed, which has changed at an interval of 9 years after destabilization in the range of Po = 11.95…3.63…5.06 sec. It was also established that the precession period during the same time varied within Рpr = 71.0…234.0 …226.0 sec. The angle of the precession of the axis of rotation relative to the direction from the center of the satellite to the center of the Earth is within 38°…28°.
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