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Relative equilibria of dynamically symmetric CubeSat nanosatellite under the action of aerodynamic and gravitational torques
Barinova E.V., Timbai I.A.
Assessment of the possibility of shortening the landing distance of maneuverable aircraft
Strelets M.Y., Tarasov A.Z., Grishin I.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.
Optimization of trajectory motion of the first stage of an aerospace system
Khramov A.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.
Method and technical tools of assessing the reliability of digital angle converters
Grechishnikov V.M., Yudin A.A.
Thermal control of spacecraft star sensor attitude control system based on the solution of a coupled thermoelasticity problem
Tsaplin S.V., Bolychev S.A.
Comparing of modeling methods of X-RAY radiation propagation in paraxial area
Nalimov A.G., Khonina S.N.
The effectiveness of using multispectral and hyperspectral remote sensing data for environmental monitoring
Anshakov G.P., Zhuravel Y.N., Fedoseev A.A.
Development of methods of modeling and computer-aided design of compressors
Krivosheev I.A., Rozhkov K.E.
Cycle parameters of an internal combustion spark-ignition gas piston engine with an electronic control system
Shishkov V.A.
The oretical substantiation of the constructive scheme of the air-gas tract rinsing device for GTE
Silaev B.M., Mal’tsev E.N.
Construction of limitation diagrams for truss core stiffness and strength parameters
Gainutdinov V.G., Gainutdinova T.Y., Abdullin I.N.
Analysis of the cause of serious flight accident
Vakhrushev D.E., Agaphonov O.A., Pryadko S.P., Schukin A.V.
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.
To a question on function of differential in adjustment tooth milling machine
Smolin V.D., Chigrinev I.A.
Calculation of flow characteristics of liquid fuel supplied through pressure jet atomizers of small-sized gas turbine engines
Gurakov N.I., Zubrilin I.A., Hernandez Morales M., Yakushkin D.V., Didenko A.A., Matveev S.G., Komisar Y.V.
Optimizing a vehicle trans-atmospheric motion using Pontryagin’s maximum principle
Balakin V.L., Ishkov S.A., Khramov A.A.
Determining the angle of advance of ignition when switching from petrol to gas depending on fuel mixture burning rate
Shishkov V.A.
Optimizing the propulsion of a hypersonic accelerator aircraft of a two-stage aerospace system
Balakin V.L., Bebyakov A.A., Kotchyan A.G.
Сalculation of characteristics of atomization of liquid supplied at an angle to the flow direction and justification of adjusting the angle of the nozzle inclination relative to the gas flow
Teslya D.N., Mityaev S.V., Drobyshev P.A.
Optimization of space vehicle trans-atmospheric motion by using the method of sequential linearization
Balakin V.L., Ishkov S.A., Khramov A.A.
Analysis of contact stresses in drawing round products
Kargin V.R., Kargin B.V., Kolesnikova S.Y., Sergeev Y.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.
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