A mathematical model of information and statistical synthesis of unmanned aerial vehicle on the basis of the experimental data
Authors: Koryanov V.V., Nguen V.T.
Issue: #2 (50)
Aviation and Rocket-Space Engineering
Methodological approaches to solving problems of large-scale spacecraft constellation control
Authors: Matyushin M.M., Sokolov N.L., Ovechko V.M.
Selecting the rendezvous control program of spacecraft debris collector at geostationary orbit with low transversal thrust
Authors: Ishkov S.A., Filippov G.A.
Final ascent to the geostationary orbit with the electric propulsion engine
Authors: Yakovlev A.V., Vnukov A.A., Balandina T.N.
Problems of using a prospective selection algorithm in the operational control loop for maximum descent safety in case of off-nominal situations
Authors: Kutomanov A.Yu., Kudryavtsev S.I.
A study of three-dimensional "detour" transfers into artificial lunar satellite orbit following launches from space centers located in Russia
Authors: Bychkov A.D.
Intelligent analysis technique for automated prediction of spacecraft status
Authors: Soloviev S.V.
Mechanical Engineering and Machine Science
Three-dimensional graphic interpretation of manipulator telemetry data
Authors: Kotuzhenko N.V., Savin L.A.
Developing an integrated system of the product life cycle support
Authors: Kuzin E.I., Kuzin V.E.