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Modeling the disturbing effect on the aist small spacecraft based on the measurements data

Scientific reports, 2022-01, Vol.12 (1), p.1300-1300, Article 1300

2022

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Modeling the effect of temperature deformations of large elements on the dynamics of the orbital motion of a small spacecraft

Journal of physics. Conference series, 2019-11, Vol.1368 (4), p.42074

2019

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Restoration of the current signal from solar panels of AIST small spacecraft for estimate the parameters of the rotational motion

Journal of physics. Conference series, 2020-01, Vol.1441 (1), p.12112

2020

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Analysis of micro-acceleration requirements in the context of designing a small technological spacecraft

Journal of physics. Conference series, 2021-02, Vol.1791 (1), p.12001

2021

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The simulation results of the operation of a small spacecraft motion control system with an electrothermal microdrive

Journal of physics. Conference series, 2019-11, Vol.1368 (4), p.42031

2019

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Investigation of the rotational motion stability of the aist small spacecraft prototype according to the measurements of the earth’s magnetic field

Journal of physics. Conference series, 2021-05, Vol.1901 (1), p.12022

2021

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Investigation of the dynamics of a small spacecraft elastic element temperature change under a temperature shock considering a penumbral section

IOP conference series. Materials Science and Engineering, 2021-02, Vol.1061 (1), p.12028

2021

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Alternative solutions to increase the duration of microgravity calm period on board the space laboratory

Acta astronautica, 2011-09, Vol.69 (7), p.480-484

2011

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Selecting the Parameters of the Orientation Engine for a Technological Spacecraft

IOP conference series. Materials Science and Engineering, 2018-01, Vol.302 (1), p.12019

2018

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Dynamic characteristics modeling of rotary platform installed on board of a small spacecraft

Journal of physics. Conference series, 2022-03, Vol.2182 (1), p.12061

2022

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Problems in formation and control of a required microacceleration level at spacecraft design, tests, and operation

Russian aeronautics, 2014-04, Vol.57 (2), p.111-117

2014

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Evaluation of the Effect of the Difference between the Real Attachment Unit and the Sealing in the Study of the Stress-Strain State of the Solar Panel of a Small Spacecraft as a Result of a Temperature Shock

Applied Mechanics and Materials, 2022-01, Vol.904, p.27-33

2022

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Probabilistic estimation of fulfilling favorable conditions to realize the gravity-sensitive processes aboard a space laboratory

Russian aeronautics, 2013-07, Vol.56 (3), p.297-302

2013

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The Techniques to Control a Space Laboratory Orbital Motion During Conducting of Gravity-sensitive Processes on Its Board

American journal of aerospace engineering (Print), 2016, Vol.3 (1), p.6

V. Sedelnikov, A.

2016

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Fractal assessment of microaccelerations at weak damping of natural oscillation in spacecraft elastic elements. II

Russian aeronautics, 2007-09, Vol.50 (3), p.322-325

Sedel'nikov, A V

2007

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Simulation of a flexible spacecraft motion to evaluate microaccelerations

Russian aeronautics, 2009-12, Vol.52 (4), p.484-487

2009

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A problem of choosing a generalized parameter of flexible spacecraft structures to construct a fractal model of microaccelerations

Russian aeronautics, 2008-03, Vol.51 (1), p.84-86

Sedel’nikov, A. V.

2008

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Algorithm for the Operation of the Data-Measuring System for Evaluating the Inertial-Mass Characteristics of Space Debris

7th International Conference on Computing, Control and Industrial Engineering (CCIE 2023), p.1087-1093

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The problem of estimating microaccelerations aboard Foton-M4 spacecraft

Russian aeronautics, 2017, Vol.60 (1), p.83-89

2017

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Effect of the Mission and Supporting Equipment on Operation of the Magnetometer Sensors of the Foton-M No. 2 Spacecraft

Russian aeronautics, 2019-10, Vol.62 (4), p.571-576

2019

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Efficiency Estimation of Electrothermal Thrusters Use in the Control System of the Technological Spacecraft Motion

Russian aeronautics, 2018-07, Vol.61 (3), p.347-354

2018

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Modulation of gas laser radiation by an alternating magnetic field

Soviet journal of quantum electronics, 1975-04, Vol.5 (4), p.436-439

1975

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Concerning the sensitivity of the method of determining the dispersion width of the atomic-transition line in a gas laser to the excitation level

Radiophysics and quantum electronics, 1974-02, Vol.17 (2), p.160-164

1974

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Modulation of the radiation frequency of a gas laser by modulation of the relative excitation

Radiophysics and quantum electronics, 1971-09, Vol.14 (9), p.1049-1053

1971

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Forecasting the Impact of Investments on Spatial Heterogeneity in the Development of the Livestock Industry

Economic and social changes, 2023 (2 (86))

2023

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Modeling the disturbing effect on the aist small spacecraft based on the measurements data

Modeling the effect of temperature deformations of large elements on the dynamics of the orbital motion of a small spacecraft

Restoration of the current signal from solar panels of AIST small spacecraft for estimate the parameters of the rotational motion

Analysis of micro-acceleration requirements in the context of designing a small technological spacecraft

The simulation results of the operation of a small spacecraft motion control system with an electrothermal microdrive

Investigation of the rotational motion stability of the aist small spacecraft prototype according to the measurements of the earth’s magnetic field

Investigation of the dynamics of a small spacecraft elastic element temperature change under a temperature shock considering a penumbral section

Alternative solutions to increase the duration of microgravity calm period on board the space laboratory

Selecting the Parameters of the Orientation Engine for a Technological Spacecraft

Dynamic characteristics modeling of rotary platform installed on board of a small spacecraft

Problems in formation and control of a required microacceleration level at spacecraft design, tests, and operation

Evaluation of the Effect of the Difference between the Real Attachment Unit and the Sealing in the Study of the Stress-Strain State of the Solar Panel of a Small Spacecraft as a Result of a Temperature Shock

Probabilistic estimation of fulfilling favorable conditions to realize the gravity-sensitive processes aboard a space laboratory

The Techniques to Control a Space Laboratory Orbital Motion During Conducting of Gravity-sensitive Processes on Its Board

Fractal assessment of microaccelerations at weak damping of natural oscillation in spacecraft elastic elements. II

Simulation of a flexible spacecraft motion to evaluate microaccelerations

A problem of choosing a generalized parameter of flexible spacecraft structures to construct a fractal model of microaccelerations

Algorithm for the Operation of the Data-Measuring System for Evaluating the Inertial-Mass Characteristics of Space Debris

The problem of estimating microaccelerations aboard Foton-M4 spacecraft

Effect of the Mission and Supporting Equipment on Operation of the Magnetometer Sensors of the Foton-M No. 2 Spacecraft

Efficiency Estimation of Electrothermal Thrusters Use in the Control System of the Technological Spacecraft Motion

Modulation of gas laser radiation by an alternating magnetic field

Concerning the sensitivity of the method of determining the dispersion width of the atomic-transition line in a gas laser to the excitation level

Modulation of the radiation frequency of a gas laser by modulation of the relative excitation

Forecasting the Impact of Investments on Spatial Heterogeneity in the Development of the Livestock Industry

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