Influence of the End Body Dynamics on Stabilization Processes in the Relative Motion of a Space Tethered System Stabilized by Rotation

Authors

  • O.L. Volosheniuk Institute of Technical Mechanics, the NAS of Ukraine and the State Space Agency of Ukraine

DOI:

https://doi.org/10.15407/scine15.02.015

Keywords:

mathematical model, space tethered system, stabilization by rotation, stabilization processes

Abstract

Introduction. Space tethered systems (STS) stabilized by rotation is a quite interesting and promising direction in the field of cosmonautics. Such systems are intended for solving a wide range of scientific and research tasks, in particular, those that cannot be solved effectively with the help of the existing space technologies, for example, transport operations, creation of artificial gravity, removal of space debris objects, obtainment of experimental data of functioning tethered systems, etc.
Problem Statement. The peculiarities of the STS dynamics models are determined by the specifics of the problems solved by such systems actual among which is the researches the effects of the end body dynamics on the system motion.
Purpose. To build a mathematical model of the STS dynamics for considering the general regularities of the system motion and to analyze comprehensively the special features of the end body dynamics.
Materials and Methods. The mathematical model of the STS dynamics has been built based on the methods and principles of theoretical mechanics and space flight dynamics. To study the STS dynamics, methods of the theory of oscillations, analytical and numerical integration of differential motion equations have been used.
Results. The simplest model of the STS dynamics consisting of the material point and the end body connected by a tether is presented for the motion under consideration. The possibility of the appearance of internal resonances and their influence on the stabilization processes in the relative motion of the system has been considered.
Conclusions. The proposed model can apply to analyzing the angular oscillation of the end body relative to the tether attachment point, taking into account the effects of the inertial characteristics of the end body, the tether stiffness and the angular velocity of the proper rotation of the system. Practical problems related to the STS dynamics may include the problems of the stability of the end body orientation, resonance modes in the system motion, as well as the problems in creating the prerequisites for the design of the specific STS.

References

Linskens, H. T. K., Mooij, E. (2016). Tether Dynamics Analysis and Guidance and Control Design for Active Space-Debris Removal. Journal of Guidance, Control, and Dynamics, 39(6), 1232-1243.

https://doi.org/10.2514/1.G001651

Cartmell, M. P., McKenzie, D. J. (2008). A review of Space Tether research. Progress in Aerospace Sciences, 44(1), 1-21.

https://doi.org/10.1016/j.paerosci.2007.08.002

Volosheniuk, O. L., Pirozhenko, A. V., Khramov, D. A. (2011). Space Tethered Systems - a promising trend in the sphere of space engineering and technologies. Space science and Technology, 17(2), 32-44.

https://doi.org/10.15407/knit2011.02.032

Troger, H., Alpatov, А. P., Beletsky, V. V., Dranovskii, V. I., Khoroshilov, V. S., Pirozhenko, A. V., Zakrzhevskii, A. E. (2010). Dynamics of tethered space systems. Boca Raton London New York: CRC Pres. Taylor & Francis Group.

https://doi.org/10.1201/9781439836866

Levin, E. M. (2007). Dynamic analysis of space tether missions. San Diego, Calif.: Published for the American Astronautical Society by Univelt, Inc.

James, H. G., Yau, A. W., Tyc, G. (1995, April). Space research in the BICEPS experiment. Fourth International Conference on tether in Space, Washington. P. 1585–1598.

Volosheniuk, О. L., Pirozhenko, A. V. (2004). Mathematical model of dynamics of a space tethered system subjected to spin stabilization. Technical Mechanics, 2, 17–27 [in Russian].

Volosheniuk, О. L., Pirozhenko, A. V. (2005). Analysis of Frequencies and Characteristics of Transient Responses of a Space Tethered System Stabilized by Rotation. Technical Mechanics, 1, 13–21 [in Russian].

Beletskiy, V. V. (2009). Profiles on Movement of Space Bodies. Мoscow: Publishing house LKI [in Russian].

Downloads

Published

2024-09-04

How to Cite

Volosheniuk, O. (2024). Influence of the End Body Dynamics on Stabilization Processes in the Relative Motion of a Space Tethered System Stabilized by Rotation. Science and Innovation, 15(2), 15–22. https://doi.org/10.15407/scine15.02.015

Issue

Vol. 15 No. 2 (2019): Science and Innovation

Section

Scientific Basis of Innovation Activities

License

Copyright (c) 2024 Copyright Notice Authors published in the journal “Science and Innovation” agree to the following conditions: Authors retain copyright and grant the journal the right of first publication. Authors may enter into separate, additional contractual agreements for non-exclusive distribution of the version of their work (article) published in the journal “Science and Innovation” (for example, place it in an institutional repository or publish in their book), while confirming its initial publication in the journal “Science and innovation.” Authors are allowed to place their work on the Internet (for example, in institutional repositories or on their website).

Creative Commons License

This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.