Volume 3, Issue 1-1, February 2016, Page: 6-9
The Techniques to Control a Space Laboratory Orbital Motion During Conducting of Gravity-sensitive Processes on Its Board
A. V. Sedelnikov, Departament of Space Mechanical Engineering of Samara State Aerospace University, Samara, Russia
Received: Dec. 24, 2014;       Accepted: Dec. 28, 2014;       Published: Jul. 28, 2015
DOI: 10.11648/j.ajae.s.2016030101.12      View  3898      Downloads  79
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.
Control of Orbital Motion, Level of Microaccelerations, Gravity-Sensitive Processes
To cite this article
A. V. Sedelnikov, The Techniques to Control a Space Laboratory Orbital Motion During Conducting of Gravity-sensitive Processes on Its Board, American Journal of Aerospace Engineering. Special Issue: Space Laboratories: History, Researches, Prospects. Vol. 3, No. 1-1, 2016, pp. 6-9. doi: 10.11648/j.ajae.s.2016030101.12
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.
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.
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.
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.
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.
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.
A.G. Brovkin, B.G.. Burdygov and S.V. Gordiyko Anboard control systems of spacecrafts, (Moskow, Publishing house of MAI-PRINT, 2010), p. 304.
A.V. Sedelnikov “Fractal quality of microaccelerations,” Microgravity Scienes and Technology, vol. 24, No 5, 2012, pp.345–350.
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.
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.
Patent RU 2181094 C1 29.08.2000.
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