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Title
Authors
Assessment of the possibility of shortening the landing distance of maneuverable aircraft
Strelets M.Y., Tarasov A.Z., Grishin I.A.
Optimization of trajectory motion of the first stage of an aerospace system
Khramov A.A.
Relative equilibria of dynamically symmetric CubeSat nanosatellite under the action of aerodynamic and gravitational torques
Barinova E.V., Timbai I.A.
Optimization of space vehicle combined orbital plane change maneuver on the basis of the successive linearization method
Balakin V.L., Ishkov S.A., Khramov A.A.
Deviation of reentry spacecraft from the estimated trajectory caused by transient modes of angular motion at the stage of entry into the atmosphere
Barinova Y.V., Timbay I.A.
Optimization of space vehicle combined orbital plane change maneuver on the basis of pontryagin’s maximum principle
Khramov A.A.
Command control of hypersonic aircraft angle of attack during acceleration and climb
Kotchyan A.G.
Analysis of uncontrolled motion of the “ Soyuz “ carrier rocket orbital stage after payload separation
Belokonov I.V., Storozh A.D., Timbai I.A.
Optimizing a vehicle trans-atmospheric motion using Pontryagin’s maximum principle
Balakin V.L., Ishkov S.A., Khramov A.A.
Optimizing the propulsion of a hypersonic accelerator aircraft of a two-stage aerospace system
Balakin V.L., Bebyakov A.A., Kotchyan A.G.
Optimization of space vehicle trans-atmospheric motion by using the method of sequential linearization
Balakin V.L., Ishkov S.A., Khramov A.A.
Choosing the form of space vehicle designed for descent in the rarefied atmosphere of Mars
Aslanov V.S., Ledkov A.S.
Analysis of SamSat-218D nanosatelite motion acording to trajectory measurements
Belokonov I.V., Timbai I.A., Nikolaev P.N., Orazbaeva U.M.
Efficiency of terminal control in the trans-atmospheric first stage of an aerospace system under atmospheric and aerodynamic disturbances
Balakin V.L., Kovalyov A.V., Krikunov M.M.
Command control of hypersonic cruising aircraft during climb
Balakin V.L., Kotchyan A.G.
Analysis of the influence of low-orbit nanosatellite uncontrolled motion on the possibility of solving navigation and communication problems after its separation from the «Soyuz» carrier rocket upper-stage
Belokonov I.V., Kramlikh A.V., Timbai I.A.
1 - 16 of 16 Items

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