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Method of predictive studies of the effectiveness of spacecraft modifications with integrated subsystem replacement
Matveev Y., Lamzin V., Lamzin V.
Development of a Model of Magnetic Disturbances from Structural Elements of a Small Spacecraft and Investigation of Their Influence on the Orientation and Stabilization System
Milov A., Rozin P.
Method for Validation of the Onboard Attitude Control System Software of the Auriga Earth Remote Sensing Small Spacecraft
Rozin P.
On the problem of designing small spacecraft with electric propulsion power plants for studying minor bodies of the Solar System
Kulkov V., Egorov Y., Krainov A., Shakhanov A., Elnikov R.
The Effect on Small Spacecraft of the Shock Loading Level by Actuation of the Separation System
Demenko O., Birukov A.
Optimal Control of a Spacecraft During Descent in the Martian Atmosphere
Matjushin M., Sokolov N., Ovechko V.
Transformable descent vehicles
Pichkhadze K., Finchenko V., Aleksashkin S., Ostreshko B.
Control of Spacecraft Relative Motion in a Tandem Flight Configuration
Nazarov A.
A Numerical Study of the Force Effects of Solar Radiation on Spacecraft Surfaces Considering their Real Geometry
Shmatov S.
Comparison of some characteristics of comets 1P/Halley and 67P/Churyumov–Gerasimenko from the Vega and Rosetta mission data
Ksanfomality L.
Proposals for the construction of space systems based on small spacecraft and a transport and power module with a nuclear power plant
Barabanov A., Papchenko B., Pichkhadze K., Rebrov S., Semenkin A., Sysoev V., Yanchur S.
Features of Testing the Impact Strength of the Landing Module of the Exomars-2020 Interplanetary Vehicle
Demenko O., Biryukov A.
On Increasing the Accuracy of Star Trackers to Subsecond Levels
Zacharov A., Krusanova N., Moskatiniev I., Prohorov M., Stekol’shchikov O., Sysoev V., Tuchin M., Yudin A.
From the Vega mission to comet Halley to the Rosetta mission to comet 67/P Churyumov–Gerasimenko
Zelenyi L., Ksanfomality L.
Control of the Tandem Configuration Geometry in the Bistatic Interferometric Survey
Nazarov A.
Use of Programs for Two-Parameter Multiple Impulse Correction of Altitude and Inclination of Circular Orbits
Nazarov A.
Main methods of trajectory synthesis for scenarios of space missions with gravity assist maneuvers in the system of Jupiter and with landing on one of its satellites
Golubev Y., Tuchin A., Grushevskii A., Koryanov V., Tuchin D., Morskoy I., Simonov A., Dobrovolskii V.
A technique for processing of planetary images with heterogeneous characteristics for estimating geodetic parameters of celestial bodies with the example of Ganymede
Zubarev A., Nadezhdina I., Brusnikin E., Karachevtseva I., Oberst J.
Design of a Rational Mission Profile for the Flight of Spacecraft to the Solar System Center
Platov I., Simonov A.
On Choosing a Rational Flight Trajectory to the Moon
Gordienko E., Khudorozhkov P.
Choosing an efficient option of the combined propulsion system and flight profile of the INTERHELIO-PROBE spacecraft
Platov I., Simonov A., Konstantinov M.
Simulating the Operational Conditions of Radiative Coolers for Photo-Detectors of Optoelectronic Equipment in Ground Thermal Vacuum Tests
Goncharov K., Katin A., Korzhov K., Kupershtein V., Tulin D., Shabarchin A.
Relativistic Gravitational Experiment in the Earth Orbit: Concept, Technology, and Configuration of Satellite Constellation
Barabanov A., Milyukov V., Moskatiniev I., Nesterin I., Sysoev V., Yudin A.
The analysis of ballistic capabilities for countering disturbances associated with temporary emergency electric propulsion shutdown
Konstantinov M., Nguyen D.
Electromagnetic Interference Generated in a Spacecraft During Static Charge Accumulation
Lubomudrov A., Efanov V., Gorovtsov V., Kuzin E.
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