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Mean of Microaccelerations Estimate in the Small Spacecraft Internal Environment with the Use of Fuzzy Sets

Microgravity science and technology, 2018-08, Vol.30 (4), p.503-509

Sedelnikov, A. V.

2018

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The Assessment Problem of Microaccelerations at the Experimental Sample of the Small Spacecraft “AIST” after the Battery Degradation and the Method of its Solution

Microgravity science and technology, 2020-08, Vol.32 (4), p.673-679

Sedelnikov, A. V.

2020

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Accuracy assessment of microaccelerations simulation on the spacecraft “Foton-M” no. 2 according to magnetic measuring instruments data

Microgravity science and technology, 2020-06, Vol.32 (3), p.259-264

Sedelnikov, A. V.

2020

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Development of Control Algorithms for the Orbital Motion of a Small Technological Spacecraft with a Shadow Portion of the Orbit

Microgravity science and technology, 2020-10, Vol.32 (5), p.941-951

2020

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Analysis of the Significance of the Influence of Various Components of the Disturbance from a Temperature Shock on the Level of Microaccelerations in the Internal Environment of a Small Spacecraft

Microgravity science and technology, 2021-04, Vol.33 (2), Article 22

2021

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Construction of the Criterion for Using a Two-dimensional Thermal Conductivity Model to Describe the Stress–strain State of a Thin Plate Under the Thermal Shock

Microgravity science and technology, 2021-12, Vol.33 (6), Article 65

2021

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Modeling of Microaccelerations Caused by Running of Attitude-Control Engines of Spacecraft with Elastic Structural Elements

Microgravity science and technology, 2016-10, Vol.28 (5), p.491-498

Sedelnikov, A. V.

2016

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Classification of Microaccelerations According to Methods of their Control

Microgravity science and technology, 2015-06, Vol.27 (3), p.245-251

Sedelnikov, A. V.

2015

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The Usage of Fractal Quality for Microacceleration Data Recovery and for Measuring Equipment Efficiency Check

Microgravity science and technology, 2014-11, Vol.26 (5), p.327-334

Sedelnikov, A. V.

2014

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Fractal Quality of Microaccelerations

Microgravity science and technology, 2012-11, Vol.24 (5), p.345-350

Sedelnikov, A. V.

2012

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How to Estimate Microaccelerations for Spacecraft with Elliptical Orbit

Microgravity science and technology, 2016-04, Vol.28 (1), p.41-48

2016

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How Does Asymmetry of Solar Panels Influence Constructive Component of Microacceleration Field of Inner Environment of Space Laboratory

Microgravity science and technology, 2017-08, Vol.29 (4), p.305-311

2017

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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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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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Consideration of the Initial Deformation From Natural Oscillations of Large Elastic Elements of the Spacecraft When Assessing Microaccelerations From Thermal Shock Using a Two-dimensional Model of Thermal Conductivity

Microgravity science and technology, 2022-04, Vol.34 (2), Article 22

2022

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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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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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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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The dispersion characteristic of a three-mode gas laser for modulation of the relative excitation

Radiophysics and quantum electronics, 1973-06, Vol.16 (6), p.684-688

1973

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Synthesis and Crystal Structures of New RRuxGa1 –x (R = Er, Tm, Lu) Gallides and R2Ru1 –xIn1 +x (R = Dy, Ho, Er, Tm, Lu) Indides

Inorganic materials, 2022-06, Vol.58 (6), p.568-577

2022

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Mean of Microaccelerations Estimate in the Small Spacecraft Internal Environment with the Use of Fuzzy Sets

The Assessment Problem of Microaccelerations at the Experimental Sample of the Small Spacecraft “AIST” after the Battery Degradation and the Method of its Solution

Accuracy assessment of microaccelerations simulation on the spacecraft “Foton-M” no. 2 according to magnetic measuring instruments data

Development of Control Algorithms for the Orbital Motion of a Small Technological Spacecraft with a Shadow Portion of the Orbit

Analysis of the Significance of the Influence of Various Components of the Disturbance from a Temperature Shock on the Level of Microaccelerations in the Internal Environment of a Small Spacecraft

Construction of the Criterion for Using a Two-dimensional Thermal Conductivity Model to Describe the Stress–strain State of a Thin Plate Under the Thermal Shock

Modeling of Microaccelerations Caused by Running of Attitude-Control Engines of Spacecraft with Elastic Structural Elements

Classification of Microaccelerations According to Methods of their Control

The Usage of Fractal Quality for Microacceleration Data Recovery and for Measuring Equipment Efficiency Check

Fractal Quality of Microaccelerations

How to Estimate Microaccelerations for Spacecraft with Elliptical Orbit

How Does Asymmetry of Solar Panels Influence Constructive Component of Microacceleration Field of Inner Environment of Space Laboratory

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

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

Consideration of the Initial Deformation From Natural Oscillations of Large Elastic Elements of the Spacecraft When Assessing Microaccelerations From Thermal Shock Using a Two-dimensional Model of Thermal Conductivity

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

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

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

The dispersion characteristic of a three-mode gas laser for modulation of the relative excitation

Synthesis and Crystal Structures of New RRuxGa1 –x (R = Er, Tm, Lu) Gallides and R2Ru1 –xIn1 +x (R = Dy, Ho, Er, Tm, Lu) Indides

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