Modeling and analysis of the process of forming a vertical tether group of nano-satellites

C. Q. Wang; Y. M. Zabolotnov

doi:10.1088/1742-6596/1096/1/012196

Modeling and analysis of the process of forming a vertical tether group of nano-satellites

C. Q. Wang, Y. M. Zabolotnov

Research output: Contribution to journal › Conference article › peer-review

Abstract

The task of forming a tether group of nano-satellites in a circular orbit near the Earth is considered. The tether system consists of the basic spacecraft and several nanosatellites. Nominal programs for the deployment of the tether system in the vertical position according to the simplified equations of motion are constructed.The feasibility of the obtained programs for the development of the tether system for a more complex model of motion is confirmed. Example of forming a tether system consisting of the basic spacecraft and ten nano-satellites is provided.

Original language	English
Article number	012196
Journal	Journal of Physics: Conference Series
Volume	1096
Issue number	1
DOIs	https://doi.org/10.1088/1742-6596/1096/1/012196
State	Published - 11 Dec 2018
Externally published	Yes
Event	4th International Conference on Information Technology and Nanotechnology, ITNT 2018 - Samara, Russian Federation Duration: 24 Apr 2018 → 27 Apr 2018

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10.1088/1742-6596/1096/1/012196

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title = "Modeling and analysis of the process of forming a vertical tether group of nano-satellites",

abstract = "The task of forming a tether group of nano-satellites in a circular orbit near the Earth is considered. The tether system consists of the basic spacecraft and several nanosatellites. Nominal programs for the deployment of the tether system in the vertical position according to the simplified equations of motion are constructed.The feasibility of the obtained programs for the development of the tether system for a more complex model of motion is confirmed. Example of forming a tether system consisting of the basic spacecraft and ten nano-satellites is provided.",

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N2 - The task of forming a tether group of nano-satellites in a circular orbit near the Earth is considered. The tether system consists of the basic spacecraft and several nanosatellites. Nominal programs for the deployment of the tether system in the vertical position according to the simplified equations of motion are constructed.The feasibility of the obtained programs for the development of the tether system for a more complex model of motion is confirmed. Example of forming a tether system consisting of the basic spacecraft and ten nano-satellites is provided.

AB - The task of forming a tether group of nano-satellites in a circular orbit near the Earth is considered. The tether system consists of the basic spacecraft and several nanosatellites. Nominal programs for the deployment of the tether system in the vertical position according to the simplified equations of motion are constructed.The feasibility of the obtained programs for the development of the tether system for a more complex model of motion is confirmed. Example of forming a tether system consisting of the basic spacecraft and ten nano-satellites is provided.

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Modeling and analysis of the process of forming a vertical tether group of nano-satellites

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