设计回收太空碎片的机器人飞行器

IF 0.4 Q4 ENGINEERING, MECHANICAL
M. E. Barkova, A. O. Zhukov, I. N. Kartsan, V. O. Kuznetsova, D. V. Ulanov, I. N. Kravchenko, O. V. Barmina
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引用次数: 0

摘要

摘要收集空间碎片的航天器的概念假定,它的轨道随着空间碎片在不同轨道上的位置而不断变化。在轨道高度为 800-1000 公里和 1400-1500 公里、倾角为 60-80° 的轨道上观测到的空间碎片密度最高,为 10-6 吨/立方公里。为此,应确定茹科夫斯基意义上的稳定轨道。我们提出了一种利用朱可夫斯基意义上的轨迹稳定性定理选择空间碎片收集器(包括机器人航天器)轨道的方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

Designing a Robotic Vehicle for Recycling Space Debris

Designing a Robotic Vehicle for Recycling Space Debris

Designing a Robotic Vehicle for Recycling Space Debris

The concept of a spacecraft for collecting space debris assumes that its orbit continuously changes in relation to the location of space debris in various orbits. The highest density of space debris, which is 10–6 t/km3, is observed at orbital altitudes of 800–1000 and 1400–1500 km with an inclination of 60°–80°. To this end, stable trajectories in the sense of Zhukovskii should be determined. We propose a method for selecting the orbit of a space debris collector, including a robotic spacecraft, using the theorem on the stability of trajectories in the sense of Zhukovskii.

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来源期刊
CiteScore
0.80
自引率
33.30%
发文量
61
期刊介绍: Journal of Machinery Manufacture and Reliability  is devoted to advances in machine design; CAD/CAM; experimental mechanics of machines, machine life expectancy, and reliability studies; machine dynamics and kinematics; vibration, acoustics, and stress/strain; wear resistance engineering; real-time machine operation diagnostics; robotic systems; new materials and manufacturing processes, and other topics.
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