Abstract
Thisarticle deals with new classification of microaccelerations which appear in the indoor environment of spacecraft during its exploitation. This classification allows effective application of different methods to control mocroacceleration level in the area with technological equipment with the purpose of creating of facilities to conduct gravity-sensitive processes on a board of spacecraft.
This is a preview of subscription content, log in via an institution to check access.
Similar content being viewed by others
References
Belousov, A.I., Sedelnikov, A.V.: Problems in formation and control of a required microacceleration level at spacecraft design, tests, and operation. Russian Aeronautics 57(2), 111–117 (2014)
Bezglasnyi, S.P.: Active orientation of a gyrostat with variable moments of inertia. J. Appl. Math. Mech. 78 (6), 766–777 (2014)
Blinov, V.N., Shalay, V.V., Hodoreva, E.V., et al.: Assessment of mass efficiency of the maneuvering small spacecrafts with the propulsion system of microdraft on ammonia. Omsk Scientific Bulletin 1, 59–61 (2012)
Boguslavsky, A.A., Glotov, Yu.N., Levtov, V.L., Romanov, V.V., Sazonov, V.V., Sokolov, S.M.: Numerical processing of results of experiment Dynamics-M made onboard spacecraft Foton M-3, A preprint of institute of applied mathematics of M.V. Keldysh of the Russian Academy of Sciences. (65) (2008)
Boguslavsky, A.A., Sazonov, V.V., Sokolov, S.M., Zemskov, V.S., Raukhman, M.R., Shalimov, V.P.: About influence of microaccelerations on distribution of impurity in crystals of InSb:Te which are grown up in orbital flight by method of bestigelny zonal melting. Cosm. Res. 42(2), 155–161 (2004)
Dokuchayev, L.V.: Nonlinear dynamics of aircraft with deformable elements, p 287. Mashinostroenie, Moskow (1987)
Doroshin, A.V., Neri, F.: Open research issues on nonlinear dynamics, dynamical systems and processes. WSEAS Trans. Syst. 13, 644–647 (2014)
Hughes, P.C.: Dynamics of flexible space vehicles with active attitude control. Celest. Mech. 9(1), 21–39 (1974)
Ignatov, A.I., Sazonov, V.V.: The modes of a rotary motion of an artificial satellite with the small level of residual microaccelerations. Messenger of the Nizhny Novgorod university of N.I. Lobachevsky 4(5), 2195–2197 (2011)
Ishlinsky, A.Yu.: Mechanic of the relative movement and force of inertia, p 191. Science, Moskow (1981)
Likins, P.W.: Quasicoordinate equations for flexible spacecraft. AIAA 13(4), 524–526 (1975)
Lobykin, A.A.: Methods of improvement of a microgravitational situation onboard the automatic spacecraft intended for microgravitational researches, Surface. X-ray, sinkhrotronny and neutron researches 2, 84–91 (2009)
Lubimov, V.V., Malyshev, V.I., Syomkin, N.D.: Control of a small satellite orientation with due regard to failures in the discharging system of the flywheel kinematic momenta. Giroskopiya and navigation 2, 31–41 (2013)
Meirovitch, L.: Attitude stability of an elastic body of revolution in space. J. Astronaut. Sci. 8(4), 110–113 (1961)
Riaboukha, S.B., Kiselev, S.V.: Some features of vibrational perturbations onboard the MIR orbital station. Cosm. Res. 39(2), 129–135 (2001)
Sazonov, V.V.: Gravitational orientation of artificial satellites from girodina. Cosm. Res. 26(2), 315–317 (1988)
Sazonov, V.V., Chebukov, S.Yu., Abrashkin, V.I., Kazakova, A.E., Zaitsev, A.S.: The analysis of low-frequency microaccelerations onboard the spacecraft. Cosm. Res. 39(4), 419–435 (2001)
Sedelnikov, A.V.: Fractal assessment of microaccelerations at weak damping of natural oscillation in space vehicles elastic elements. Russian Aeronautics 50(3), 322–325 (2007)
Sedelnikov, A.V.: Fractal quality of microaccelerations. Microgravity Scienes and Technology 24(5), 345–350 (2012)
Sedelnikov, A.V.: The problem of microaccelerations: from comprehension up to fractal model, p 277. Russian Academy of Sciences: The Elected Works of the Russian school, Moscow (2012)
Sedelnikov, A.V.: The usage of fractal quality for microacceleration data recovery and for measuring equipment efficiency check. Microgravity Scienes and Technology 26(5), 327–334 (2014)
Sedelnikov, A.V.: Control of microaccelerations as the major characteristics of space laboratory of specialized technological appointment as constructive methods, Testing. Diagnistics 7, 57–63 (2014)
Sedelnikov, A.V., Kireeva, A.A.: Alternative solutions to increase the duration of microgravity calm period on board the space laboratory. Acta Astronautica 69, 480–484 (2011)
Titov, B.A., Vyyuzhanin, V.A., Dmitriyev, V.V.: Formation of the dynamic properties of elastic spacecrafts, p 304. Mashinostroenie, Moskow (1995)
Zemskov, V.S., Raukhman, M.R., Shalimov, V.P.: etc., Influence of an arrangement of growth installations onboard the spacecraft on microgravitational conditions of carrying out experiments (on the example of bestigelny zonal melting InSb:Te on FOTON-3 artificial satellite). Cosm. Res. 42(2), 144–154 (2004)
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
About this article
Cite this article
Sedelnikov, A.V. Classification of Microaccelerations According to Methods of their Control. Microgravity Sci. Technol. 27, 245–251 (2015). https://doi.org/10.1007/s12217-015-9442-0
Received:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s12217-015-9442-0