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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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Estimating the Inertia Tensor Components of an Asymmetrical Spacecraft When Removing It from the Operational Orbit at the End of Its Active Life

Sensors (Basel, Switzerland), 2023-12, Vol.23 (23), p.9615

2023

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Investigation of the Stress-Strain State of a Rectangular Plate after a Temperature Shock

Mathematics (Basel), 2023-01, Vol.11 (3), p.638

2023

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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 dependence modeling of the caterpillar eggs yield of the laboratory population of Lymantria dispar on the duration of diapause

International journal of modeling, simulation and scientific computing, 2022-10, Vol.13 (5)

Sedelnikov, A. V.

2022

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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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The effect analysis of the diapause duration on the hatching parameters of the artificial semi-annual population of Lymantria dispar caterpillars

International journal of biomathematics, 2021-11, Vol.14 (8)

Sedelnikov, A. V.

2021

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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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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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Evaluation of calibration accuracy of magnetometer sensors of Aist small spacecraft

Journal of physics. Conference series, 2018-05, Vol.1015 (3), p.32045

2018

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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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Control of rotational motion of a partially inoperable small spacecraft using fuzzy sets

Journal of physics. Conference series, 2019-08, Vol.1260 (3), p.32035

2019

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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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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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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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Significance estimation of the rejected part of the signal spectrum from the magnetometer sensors of the prototype of the AIST small spacecraft

Journal of physics. Conference series, 2019-10, Vol.1333 (6), p.62024

2019

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Estimate of parameters changing of the Lymantria dispar artificial population in different environmental conditions using the quasispecies model

International journal of modeling, simulation and scientific computing, 2020-10, Vol.11 (5), p.2050053

2020

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

Estimating the Inertia Tensor Components of an Asymmetrical Spacecraft When Removing It from the Operational Orbit at the End of Its Active Life

Investigation of the Stress-Strain State of a Rectangular Plate after a Temperature Shock

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

The dependence modeling of the caterpillar eggs yield of the laboratory population of Lymantria dispar on the duration of diapause

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

The effect analysis of the diapause duration on the hatching parameters of the artificial semi-annual population of Lymantria dispar caterpillars

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

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

Evaluation of calibration accuracy of magnetometer sensors of Aist small spacecraft

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

Control of rotational motion of a partially inoperable small spacecraft using fuzzy sets

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

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

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

Significance estimation of the rejected part of the signal spectrum from the magnetometer sensors of the prototype of the AIST small spacecraft

Estimate of parameters changing of the Lymantria dispar artificial population in different environmental conditions using the quasispecies model

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

How to Estimate Microaccelerations for Spacecraft with Elliptical Orbit

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