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Title
Authors
Digital model of the drag force of the Earth’s upper atmosphere for the design of low-orbit spacecraft
Volotsuev V.V.
Methodical and algorithmic aspects of mathematical modeling of a screw aircraft power plant
Zinenkov Y.V.
Comparative results of computational and theoretical study of the annular nozzle with a flat central body
Kirshina A.A., Levikhin A.A., Kirshin A.Y.
Optimization of trajectory motion of the first stage of an aerospace system
Khramov A.A.
Programs of time-optimal control in the problem of rendezvous transfer of spacecraft with low transversal thrust
Ishkov S.A., Filippov G.A., Fadeenkov P.V.
Approximate methods of calculating optimal flights of space vehicles with low-thrust engines. Part II
Salmin V.V., Vassiliev V.V., Ishkov S.A., Romanenko V.A., Sokolov V.O., Starinova O.L., Yurin V.V.
Оptimization of gas turbine aircraft engine control throughout the engine service life
Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.
The usage of high power supply capacity transport spacecraft
Ivanovich S.N.
Iteration procedure of choosing a low-thrust rendezvous transfer control program in problems of space debris disposal in the geostationary orbit
Philippov G.A.
Control of in-plane orbit parameters of a geostationary low-thrust satellite
Salmin V.V., Chetverikov A.S.
Optimum programs of correction of quasielliptical and circular orbits of spacecraft with the limited-thrust engine
Khramov A.A.
Optimal control of spacecraft motion in the vicinity of Eros 433 asteroid
Shornikov A.Y.
Optimization methods of design-ballistic characteristics circumterraneous and interplanetary space vehicle with electrojet engines of low thrust
1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1.
Selection of project structure for nanosatellite propulsion system
Belokonov I.V., Ivliev A.V., Bogatyrev A.M., Kumarin A.A., Lomaka I.A., Simakov S.P.
Firing test stand pulse detonation low-thrust engines
Govorenkho G.S., Teterin D.P., Kotelnikhov D.S., Aliluev A.V., Aliluev S.V., Fedorets V.N.
Propulsion systems and low-thrust rocket engines based on various physical principles for control systems of small and micro-spacecraft
Ryzhkov V.V., Sulinov A.V.
System of artificial intellect support of low-thrust spacecraft interplanetary mission optimization
Starinova O.L.
1 - 17 of 17 Items

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