space flight mechanics, re-entry ballistics and spacecraft attitude dynamics, space tethered systems and space elevator dynamics, space debris mitigation, general problems of the regular and chaotic synamics.
Aslanov, V.S., Ledkov, A.S., “Dynamics of towed large space debris taking into account atmospheric disturbance”, Doi: 0.1007/s00707-014-1094-4, Acta Mechanica, 225:9 (2014), 2685-2697
Aslanov V.S., Ledkov A.S., “Tether-assisted re-entry capsule deorbiting from an elliptical orbit”, Doi: 10.1016/j.actaastro.2016.10.028, Acta Astronautica, 130 (2017), 180–186
Aslanov, V.S., Ledkov, A.S., “Chaotic motion of a reentry capsule during descent into the atmosphere”, Doi: 10.2514/1.G000411, Journal of Guidance, Control, and Dynamics, 39:8 (2016), 1834-1843
Aslanov V.S., Ledkov A.S., “Attitude Motion of Cylindrical Space Debris during Its Removal by Ion Beam”, https://www.hindawi.com/journals/mpe/2017/1986374/, Mathematical Problems in Engineering, 2017:1986374 (2017)
A. S. Ledkov, A. A. Belov, “Damping of out-of-plane oscillations of a spherical object during contactless transportation by an ion beam”, Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2024, no. 89, 89–102
2023
2.
A. S. Ledkov, R. S. Pikalov, “Nonlinear Control of Tether Retrieval in an Elliptical Orbit”, Rus. J. Nonlin. Dyn., 19:2 (2023), 201–218
2019
3.
V. V. Ryazanov, A. S. Ledkov, “Descent of nanosatellite from low Earth orbit by ion beam”, Izv. Saratov Univ. Math. Mech. Inform., 19:1 (2019), 82–93
A. S. Ledkov, R. G. Sobolev, “Mathematical simulation of a tethered satellite system motion with an inflatable spherical balloon during a spacecraft orbit injection”, Vestn. Tomsk. Gos. Univ. Mat. Mekh., 2018, no. 52, 63–74
A. S. Ledkov, D. I. Dyukov, “Research of consequences of tether's jamming in the task of payload delivery from an orbit”, Izv. Saratov Univ. Math. Mech. Inform., 12:3 (2012), 82–87
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