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Issue
Title
Authors
Vol 14, No 4 (2015)
Choosing a program for controlling the deployment of an orbital tether system with deployment speed limitations
Ishkov S.A., Xiaoye X., Filippov G.A.
PDF
(Rus)
Vol 16, No 2 (2017)
Control over the deployment of an orbital tether system of great length
Wang C., Zabolotnov Y.M.
PDF
(Rus)
Vol 15, No 1 (2016)
Modeling orbital tether system deployment with limitations on the deployment speed
Ishkov S.A., Filippov G.A., Xiaoye X.
PDF
(Rus)
Vol 9, No 1 (2010)
Solving the problem of stabilizing program deployment of an orbital tether system taking into account limitations on the rotary motion of the tip body
1 1., 1 1.
PDF
(Rus)
Vol 15, No 2 (2016)
Analysis of motion stability of a deployed space tether system with an atmospheric probe
Zhe D., Zabolotnov Y.M., Changqing W.
PDF
(Rus)
Vol 9, No 1 (2010)
Statistical analysis of a capsule’s motion during its reentry into the atmosphere with the aid of a space tether system
1 1., 1 1.
PDF
(Rus)
Vol 8, No 4 (2009)
Chaotic motion of the elastic tether system
Aslanov V.S., Pirozhenko A.V., Ivanov B.V., Ledkov A.S.
PDF
(Rus)
Vol 15, No 1 (2016)
Optimal stabilization of small spacecraft angular motion in the process of deployment of an orbital tether system
Zabolotnov Y.M., Lobankov A.A.
PDF
(Rus)
Vol 7, No 1 (2008)
Orbital tether system motion equations considering space vehicle vibrations
Aslanov V.S., Stratilatov N.R.
PDF
(Rus)
Vol 21, No 3 (2022)
Formation of a rotating ring-shaped three-body tethered nanosatellite system with limited control
Chen S., Zabolotnov Y.M.
PDF
(Rus)
Vol 11, No 2 (2012)
The influence of tether jamming on the motion of a space tether system during dynamic deployment
Ledkov A.S., Dyukov D.I.
PDF
(Rus)
Vol 20, No 2 (2021)
Deployment and stabilization of the motion of a space tethered system in a lunar orbit
Ledkova T.A., Zabolotnov Y.M.
PDF
(Rus)
Vol 11, No 2 (2012)
Dynamics of towing tethered spacecraft in the central gravitational field
Aslanov V., Yudintsev V.V.
PDF
(Rus)
Vol 19, No 1 (2020)
Optimizing the process of changing spacecraft orbital parameters by using a spinning electrodynamic tether sytem
Lu H., Wang C., Zabolotnov Y.M.
PDF
(Rus)
Vol 9, No 2 (2010): Special Issue
Tether parameters consideration during motion simulation of orbital tether system
1 1.
PDF
(Rus)
1 - 15 of 15 Items

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