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Methodology of delivering space parts, tools and accessories to a near Earth orbital station on the basis of the reliability factor
Zheleznov I.V., Uperchuk R.A., Eroshenko V.K.
Control over the deployment of an orbital tether system of great length
Wang C., Zabolotnov Y.M.
Optimal stabilization of small spacecraft angular motion in the process of deployment of an orbital tether system
Zabolotnov Y.M., Lobankov A.A.
Method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filter
Ananenko V.M., Golyakov A.D., Kalabin P.V.
Methods of validation of the ballistic structure of space surveillance system orbital segment
Fadin I.A., Yanov S.V., Samokhvalov O.A.
Tether parameters consideration during motion simulation of orbital tether system
1 1.
Development of methods for ensuring energy balance for the operation of mission equipment of “AIST”-series small satellites under conditions of power limitations
Ivanushkin M.A., Salmin V.V., Tkachenko S.I., Tkachenko I.S., Volgin S.S.
Possibility of using leo satellite communication systems for on-line data interchange
Davydov D.D.
Modeling orbital tether system deployment with limitations on the deployment speed
Ishkov S.A., Filippov G.A., Xiaoye X.
1 - 9 of 9 Items

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