Analysis of optimal three-impulse transfer to an artificial lunar satellite orbit
Authors: Gordienko E.S., Ivashkin V.V.
Issue: #3 (51)
Aviation and Rocket-Space Engineering
Investigating precision capabilities of a system of terminal guidance algorithms for prospective manned spacecraft during final descent phase in the Earth’s atmosphere
Authors: Kudryavtsev S.I.
Analysis of current situation in monitoring processes for spacecraft flight control
Authors: Soloviev S.V., Mishurova N.V.
Some aspects of solving the optimal control problem on the basis of the maximum principle for non-coplanar interorbital transfer
Authors: Kiriliuk E.V., Stepanov M.N.
Analysis of the mutual evolution of the parameters of two synchronous precessing orbits
Authors: Ulybyshev S.Yu.
A system of multi-level impulse correction
Authors: Velikiy Yu.V., Klishin A.N.
Study the possibility of indirect flight into the restricted orbit around the Earth-Moon’s L2 libration point
Authors: Guskova M.S., Bober S.A., Aksenov S.A.
Orbit group availability assessment
Authors: Matveyev I.V., Vovchenko S.P.
Power, Metallurgic and Chemical Engineering
Feasibility analysis of the installation for the nitrogen liquefaction
Authors: Khutsieva S.I., Mitruzaev A.E., Parkin A.N., Brom A.E.