利用光曲线估计低轨道碎片的形状和运动

T. Yanagisawa, H. Kurosaki, A. Nakajima
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引用次数: 52

摘要

我们仅利用光学望远镜获得的光曲线数据,成功地确定了一个LEO碎片Cosmos 2082火箭体的三轴椭球模型、其在天球中的旋转轴方向、组成参数、自转周期和岁差。近地轨道碎片的亮度被监测了2天。采用最小二乘拟合的方法来确定这些值。推导出LEO碎片的轴向比为100:18:18,在天球内的旋转轴方向坐标为R.A. = 305.80, dec = 2.60,其旋转周期为41秒。考虑岁差时,其幅值为30.50 min,岁差周期为29.4 min。这些结果表明,光学光曲线数据足以确定近地轨道碎片的形状和运动。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Shape and Motion Estimate of LEO Debris Using Light Curves
We succeeded in determining a tri-axial ellipsoidal model of one LEO debris Cosmos 2082 rocket body, its rotational axis direction in the celestial sphere, a compositional parameter, its rotation period and its precession using only light curve data that was obtained by an optical telescope. The brightness of the LEO debris was monitored for 2 days. The method of the least squares fitting is applied to determine these values. The derived axial ratios of the LEO debris is 100:18:18, the coordinates of the rotational axis direction in the celestial sphere are R.A. = 305.8o and Dec. = 2.6o and its rotation period is 41 seconds. When the precession is considered, its amplitude and precession period are 30.5o and 29.4 minutes, respectively. These results show that optical light curve data are sufficient to determine the shape and the motion of LEO debris.
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