Vladimir Aslanov
Full Professor, Head of Theoretical Mechanics Department.
Diploma with Honors of Aircraft Engineer, Kuibyshev Aviation Institute, Kuibyshev/ USSR, 1966-1972. Engineer, Kuibyshev Aviation Institute, Kuibyshev/ USSR, 1972-1978. Postgraduate student, Kuibyshev Aviation Institute, Kuibyshev/ USSR, 1974-1977. Instructor, Kuibyshev Aviation Institute, Kuibyshev/ USSR, 1978-1982. Associate Professor, Kuibyshev Aviation Institute, Kuibyshev/ USSR, 1982-1989. Full Professor, Head of Theoretical Mechanics Department, Samara National Research University, Samara, Russia, 1989 - present.Professor V. S. Aslanov in 2010-2014 occupies the first position in the world rankings in the distinctive competency "Spacecraft; Satellites; Control" of Samara University (the data are taken from the integrated modular platform resource Elsevier SciVal). Rewiever for Jounans: Acta Astronautica, Advances in Space Research, Aerospace Science and Technology, International Journal of Non-Linear Mechanics, Acta Mechanica, Celestial Mechanics and Dynamical Astronomy, Nonlinear Dynamics, The Aeronautical Journal. Expert, Scientific Research Institute - Federal Research Centre for Projects Evaluation and Consulting Services, 2014-present. Member of the Editorial Board of a multidisciplinary international peer reviewed journal "Annual Review of Chaos Theory, Bifurcations and Dynamical Systems", 2011-present. Expert, the Federal Agency of Education at the Ministry of Education and Science of the Russian Federation, 2009-present. Member of the Advisory Committee on Mathematics, Mechanics and computer science of the Russian Foundation for Basic Research, Moscow/Russia, 2012-present. Member, Mathematics and Mechanics Education Methodology Council of Russian Universities, Moscow/Russia, 2004-present. Member, Scientific Advisory Board for Awarding Doctoral Degrees in Ballistics, Samara/Russia, 1996-present. Member, Scientific Advisory Board for Awarding Doctoral Degrees in Mechanics, Samara/Russia, 1996-present.
Publications:
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Doroshin A. V., Aslanov V. S.
Abstract
The attitude dynamics of the Lagrange gyrostat is considered. A dynamical analogy of
the heavy Lagrange gyrostat and the magnetic Lagrange gyrostat satellite on a circle equatorial
orbit in the geomagnetic field is shown. Analytical solutions for homoclinic and heteroclinic
phase trajectories are obtained. Dynamical chaos is analyzed. The practical application of the
Lagrange gyrostat in space flight dynamics is presented. The results of the paper can be especially
applicable for small spacecraft and nanosatellites of space remote sensing constellations.
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Ledkov A. S., Neryadovskaya D. V., Aslanov V. S.
Abstract
The proposed retrieval control combats the effect of a tether winding on the end body at the
final stage of its retraction. The tether retraction rate control law providing stabilization of the
tether system is developed. The stabilization angle is determined for the fastest tether retrieval.
Unlike most works on the development of space tether retrieval control laws and schemes, this
study considers the influence of the gravitational fields of the planet and its moon. Numerical
simulation confirmed that the developed control ensures the tether retraction without a dramatic
increase in the amplitude of its oscillation at the final stage.
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