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Vol 22, No 3 (2023)

Assessment of the possibility of shortening the landing distance of maneuverable aircraft

Strelets M.Y., Tarasov A.Z., Grishin I.A.

(Rus)

Vol 23, No 1 (2024)

Optimization of trajectory motion of the first stage of an aerospace system

Khramov A.A.

(Rus)

Vol 18, No 2 (2019)

Relative equilibria of dynamically symmetric CubeSat nanosatellite under the action of aerodynamic and gravitational torques

Barinova E.V., Timbai I.A.

(Rus)

Vol 17, No 2 (2018)

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.

(Rus)

Vol 9, No 4 (2010)

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.

(Rus)

Vol 18, No 1 (2019)

Optimization of space vehicle combined orbital plane change maneuver on the basis of pontryagin’s maximum principle

Khramov A.A.

(Rus)

Vol 11, No 4 (2012)

Analysis of uncontrolled motion of the “ Soyuz “ carrier rocket orbital stage after payload separation

Belokonov I.V., Storozh A.D., Timbai I.A.

(Rus)

Vol 17, No 1 (2018)

Optimizing a vehicle trans-atmospheric motion using Pontryagin’s maximum principle

Balakin V.L., Ishkov S.A., Khramov A.A.

(Rus)

Vol 7, No 1 (2008)

Optimizing the propulsion of a hypersonic accelerator aircraft of a two-stage aerospace system

Balakin V.L., Bebyakov A.A., Kotchyan A.G.

(Rus)

Vol 16, No 3 (2017)

Optimization of space vehicle trans-atmospheric motion by using the method of sequential linearization

Balakin V.L., Ishkov S.A., Khramov A.A.

(Rus)

Vol 7, No 1 (2008)

Choosing the form of space vehicle designed for descent in the rarefied atmosphere of Mars

Aslanov V.S., Ledkov A.S.

(Rus)

Vol 18, No 4 (2019)

Analysis of SamSat-218D nanosatelite motion acording to trajectory measurements

Belokonov I.V., Timbai I.A., Nikolaev P.N., Orazbaeva U.M.

(Rus)

Vol 15, No 3 (2016)

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.

(Rus)

Vol 11, No 1 (2012)

Command control of hypersonic cruising aircraft during climb

Balakin V.L., Kotchyan A.G.

(Rus)

Vol 12, No 4 (2013)

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.

(Rus)

Vol 8, No 1 (2009)

Command control of hypersonic aircraft angle of attack during acceleration and climb

Kotchyan A.G.

(Rus)

1 - 16 of 16 Items

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