The following article deals with three different techniques to control orbital motion of spacecraft with big flexible structures during conducting of gravity-sensitive processes on its board. These processes require low level of microaccelerations. There were given examples of application of the techniques, recommendations for application of these techniques in practice, discussed advantages and disadvantages of each technique.
| Published in |
American Journal of Aerospace Engineering (Volume 3, Issue 1-1)
This article belongs to the Special Issue Space Laboratories: History, Researches, Prospects |
| DOI | 10.11648/j.ajae.s.2016030101.12 |
| Page(s) | 6-9 |
| Creative Commons |
This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited. |
| Copyright |
Copyright © The Author(s), 2015. Published by Science Publishing Group |
Control of Orbital Motion, Level of Microaccelerations, Gravity-Sensitive Processes
| [1] | A.V. Sedelnikov The Problem of Microaccelerations: from Comprehension up to Fractal Model, (Moscow, Russian Academy of Sciences: The Elected Works of the Russian School, 2012), p. 277. |
| [2] | A.I. Belousov and A.V. Sedelnikov “Problems in Formation and Control of a Required Microacceleration Level at Spacecraft Design, Tests, and Operation,” Russian Aeronautics, vol. 57, No 2, 2014, pp.111–117. |
| [3] | T. Beuselinck, Van C. Bavinchove, V.I. Abrashkin, A.E. Kazakova and V.V. Sazonov “Determination of the Spacecraft Foton M-3 Attitude Motion on Measurements of the Earth Magnetic Field,” Preprint, Keldysh Institute of Applied Mathematics, Russia Academy of Sciences, No 80, 2008. |
| [4] | A.I. Belousov and A.V. Sedelnikov “Probabilistic Estimation of Fulfilling Favorable Conditions to Realize the Gravity-sensitive Processes Aboard a Space Laboratory,” Russian Aeronautics, vol. 56, No 3, 2013, pp.297–302. |
| [5] | A.V. Sedelnikov and A.A. Kireeva “Alternative solutions to increase the duration of microgravity calm period on board the space laboratory,” Acta Astronautica, vol. 69, 2011, pp. 480–484. |
| [6] | A.V. Sedelnikov, E.Yu. Sygurova and A.A. Kireeva “The Use of Electric Engine to Reduce the Microaccelerations Level of Space lab,” Messenger the Samara State Aerospace University name of the academician of S. P. Korolev (national research university), No 3 (34), part 2, 2012, pp. 16–20. |
| [7] | A.G. Brovkin, B.G.. Burdygov and S.V. Gordiyko Anboard control systems of spacecrafts, (Moskow, Publishing house of MAI-PRINT, 2010), p. 304. |
| [8] | A.V. Sedelnikov “Fractal quality of microaccelerations,” Microgravity Scienes and Technology, vol. 24, No 5, 2012, pp.345–350. |
| [9] | A.V. Sedelnikov “The usage of fractal quality for microacceleration data recovery and for measuring equipment efficiency check,” Microgravity Scienes and Technology, vol. 26, No 5, 2014, pp.327–334. |
| [10] | V.I. Abrashkin “Preparation of the TUS space experiment for UHECR study,” International Journal of Modern Physics A, vol. 20, No 29, 2005, pp. 6865–6868. |
| [11] | Patent RU 2181094 C1 29.08.2000. |
APA Style
A. V. Sedelnikov. (2015). The Techniques to Control a Space Laboratory Orbital Motion During Conducting of Gravity-sensitive Processes on Its Board. American Journal of Aerospace Engineering, 3(1-1), 6-9. https://doi.org/10.11648/j.ajae.s.2016030101.12
ACS Style
A. V. Sedelnikov. The Techniques to Control a Space Laboratory Orbital Motion During Conducting of Gravity-sensitive Processes on Its Board. Am. J. Aerosp. Eng. 2015, 3(1-1), 6-9. doi: 10.11648/j.ajae.s.2016030101.12
AMA Style
A. V. Sedelnikov. The Techniques to Control a Space Laboratory Orbital Motion During Conducting of Gravity-sensitive Processes on Its Board. Am J Aerosp Eng. 2015;3(1-1):6-9. doi: 10.11648/j.ajae.s.2016030101.12
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Download@article{10.11648/j.ajae.s.2016030101.12,
author = {A. V. Sedelnikov},
title = {The Techniques to Control a Space Laboratory Orbital Motion During Conducting of Gravity-sensitive Processes on Its Board},
journal = {American Journal of Aerospace Engineering},
volume = {3},
number = {1-1},
pages = {6-9},
doi = {10.11648/j.ajae.s.2016030101.12},
url = {https://doi.org/10.11648/j.ajae.s.2016030101.12},
eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ajae.s.2016030101.12},
abstract = {The following article deals with three different techniques to control orbital motion of spacecraft with big flexible structures during conducting of gravity-sensitive processes on its board. These processes require low level of microaccelerations. There were given examples of application of the techniques, recommendations for application of these techniques in practice, discussed advantages and disadvantages of each technique.},
year = {2015}
}
TY - JOUR T1 - The Techniques to Control a Space Laboratory Orbital Motion During Conducting of Gravity-sensitive Processes on Its Board AU - A. V. Sedelnikov Y1 - 2015/07/28 PY - 2015 N1 - https://doi.org/10.11648/j.ajae.s.2016030101.12 DO - 10.11648/j.ajae.s.2016030101.12 T2 - American Journal of Aerospace Engineering JF - American Journal of Aerospace Engineering JO - American Journal of Aerospace Engineering SP - 6 EP - 9 PB - Science Publishing Group SN - 2376-4821 UR - https://doi.org/10.11648/j.ajae.s.2016030101.12 AB - The following article deals with three different techniques to control orbital motion of spacecraft with big flexible structures during conducting of gravity-sensitive processes on its board. These processes require low level of microaccelerations. There were given examples of application of the techniques, recommendations for application of these techniques in practice, discussed advantages and disadvantages of each technique. VL - 3 IS - 1-1 ER -
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