Sedelnikov, Andrey V.

2025

• 1 Sedelnikov A.V., Glushkov S.V., Serdakova V.V. etc. Simulating the stress-strain state of a thin plate after a thermal shock // Modeling and Simulation in Manufacturing 2025. — P. 61-70
• 2 Sedelnikov A., Glushkov S., Evtushenko M. etc. Computer Simulation of the Natural Vibrations of a Rigidly Fixed Plate Considering Temperature Shock // Computation 2025. — Vol. 13. Issue 2. № 2.

2014

• 1 Sedelnikov A.V. The Usage of Fractal Quality for Microacceleration Data Recovery and for Measuring Equipment Efficiency Check // Microgravity Science and Technology 2014. — Vol. 26. Issue 5. — P. 327-334
• 2 Belousov A. I. , Sedel'nikov A.V. Problems in formation and control of a required microacceleration level at spacecraft design, tests, and operation // Russian Aeronautics 2014. — Vol. 57. Issue 2. — P. 111-117

2006

• 1 Sedel'nikov A.V. Fractal assessment of microaccelerations at weak damping of natural oscillation in spacecraft elastic elements. I // Russian Aeronautics 2006. — Vol. 49. Issue 3. — P. 111-114

2007

• 1 Sedel'nikov A.V. Fractal assessment of microaccelerations at weak damping of natural oscillation in spacecraft elastic elements. II // Russian Aeronautics 2007. — Vol. 50. Issue 3. — P. 322-325

2008

• 1 Sedel'nikov A.V. A problem of choosing a generalized parameter of flexible spacecraft structures to construct a fractal model of microaccelerations // Russian Aeronautics 2008. — Vol. 51. Issue 1. — P. 84-86

2009

• 1 Sedel'nikov A.V., Serpukhova A.A. Simulation of a flexible spacecraft motion to evaluate microaccelerations // Russian Aeronautics 2009. — Vol. 52. Issue 4. — P. 484-487

2010

• 1 Mayasnikov S.V., SEDELNIKOV A.V., Khnyreva E.S. FORECASTING OF SALES VOLUME OF MARGARINE // European Journal of Natural History 2010. — № 6. — P. 67

2011

• 1 SEDELNIKOV A.V, Khnyreva E.S., Klimacheva I.A. Dinamcs of production indices of subsection DA in Samara regin in times of crisis // Наука в информационном пространстве Материалы VII Международной научно-практической конференции. — 2011. — P. 3-5
• 2 SEDELNIKOV A.V, Khnyreva E.S, Klimacheva I.A. Анализ динамики изменнений производства растительных и животных масел в кризисный период в Самарской области // VII Международная научно-практическая конференция Социально-экономические реформы в контексте инеграционного выбора Украины. — 2011. — P. 104-106
• 3 Sedelnikov A.V., Kireeva A.A. Alternative solutions to increase the duration of microgravity calm period on board the space laboratory // Acta Astronautica 2011. — Vol. 69. Issue 7-8. — P. 480-484

2012

• 1 Sedelnikov A.V. Fractal quality of microaccelerations // Microgravity Science and Technology 2012. — Vol. 24. Issue 5. — P. 345-350

2013

• 1 Belousov A. I. , Sedel'Nikov A.V. Probabilistic estimation of fulfilling favorable conditions to realize the gravity-sensitive processes aboard a space laboratory // Russian Aeronautics 2013. — Vol. 56. Issue 3. — P. 297-302

2015

• 1 Sedelnikov A.V., Khnyreva E.S. Исследование наличия стохастической зависимости между антикризисной монетарной поддержкой предприятий со слабой динамикой и его чистым операционным убытком // Экономические и гуманитарные науки 2015. — № № 8 (283). — P. 111-118
• 2 Sedelnikov A.V. Classification of Microaccelerations According to Methods of their Control // Microgravity Science and Technology 2015. — Vol. 27. Issue 3. — P. 245-251
• 3 Belousov A. I. , Sedelnikov A.V., Potienko K.I. Study of effective application of electric jet engine as a mean to reduce microacceleration level // International Review of Aerospace Engineering 2015. — Vol. 8. Issue 4. — P. 157-160

2024

• 1 Sedelnikov A., Skidanov R., Taneeva A. etc. Investigation of the Applicability of the Boer Formula for Estimating the Angular Velocity of Rotation Of a Small Spacecraft by Measuring the Components of The Induction Vector of the Earth's Magnetic Field in Evaluating Micro-Accelerations and Forming Control Laws // Microgravity Science and Technology 2024. — Vol. 36. Issue 6. № 6.
• 2 Sedelnikov A., Kurkin E., Kuikhada Piokuinto Kh. etc. Algorithm for Propeller Optimization Based on Differential Evolution // Computation 2024. — Vol. 12. Issue 3. № 3.
• 3 Sedelnikov A., Kurkin E., Smelov V. etc. Short Fiber-Reinforced Polymer Polyamide 6 Lugs and Selective Laser-Melted Ti-6Al-4V Bushing Contact Cohesive Zone Model Mode II Parameters’ Evaluation // Computation 2024. — Vol. 12. Issue 5. № 5.
• 4 Sedelinkov A., Nikolaeva A., Serdakova V. etc. Technologies for Increasing the Control Efficiency of Small Spacecraft with Solar Panels by Taking into Account Temperature Shock // Technologies 2024. — Vol. 12. Issue 10. № 10.
• 5 Sedelnikov A., Manukyan L., Maslowa U. The Methodology for Estimating the Angular Velocity of Rotation of a Small Spacecraft Based on a Limited Number of Magnetometric Measurements // Lecture Notes in Electrical Engineering. — 2024. — Vol. 1253 LNEE. — P. 435-440
• 6 Sedelnikov A.V., Skidanov R.V., Bratkova M.E. etc. Reconstruction of rotational motion of the ISOI (SXC3-219) small spacecraft for Earth remote sensing from onboard measurements; [Реконструкция вращательного движения малого космического аппарата дистанционного зондирования Земли ИСОИ (SXC3-219) по данным бортовых измерений] // Sovremennye Problemy Distantsionnogo Zondirovaniya Zemli iz Kosmosa 2024. — Vol. 21. Issue 5. № 5. — P. 75-82
• 7 Erisov Y., Kuzin A., Sedelnikov A. An Analytical Model for the Plastic Bending of Anisotropic Sheet Materials, Incorporating the Strain-Hardening Effect // Technologies 2024. — Vol. 12. Issue 12. № 12.
• 8 Kurkin E., Chertykovtseva V., Sedelnikov A. etc. Short-Glass-Fiber Aspect Ratios in Polyamide-6 Composites: Homogenization and Deep Learning-Based Scanning Image-Microscope Segmentation Comparison // Applied Sciences (Switzerland) 2024. — Vol. 14. Issue 23. № 23.
• 9 Kurkin E., Minaev E., Sedelnikov A. etc. Computer Vision Technology for Short Fiber Segmentation and Measurement in Scanning Electron Microscopy Images // Technologies 2024. — Vol. 12. Issue 12. № 12.
• 10 Sedelnikov A.V., Nikolaeva A.S., Serdakova V.V. etc. Approximate Solution of Initial Boundary Value Problem of One-Dimensional Heat Conduction for the Thermal Shock of Thin Plate // WSEAS Transactions on Applied and Theoretical Mechanics 2024. — Vol. 19. — P. 200-205

2016

• 1 Belousov A.I., Sedel’nikov A.V., Molyavko D.P. etc. Организация опытно-серийного производства в космосе на современном этапе // Science Review 2016. — № 17. — P. 186-194
• 2 Sedel'nikov A.V. Формализация биоцикла Lymantria dispar в модели квазивида: теоретические основы // Scientific Life 2016. — № 7. — P. 98-104
• 3 Sedelnikov A.V. Modeling of Microaccelerations Caused by Running of Attitude-Control Engines of Spacecraft with Elastic Structural Elements // Microgravity Science and Technology 2016. — Vol. 28. Issue 5. — P. 491-498
• 4 Klochkov Yu.S., Gazizulina A.Yu., A.U. Gazizulina etc. Совершенствование процедуры QFD-анализа, основанное на уточнении методов расчета значимости характеристик продукции // Известия Самарского научного центра РАН 2016. — Vol. 18. № 4 (6). — P. 1114-1120
• 5 Sedelnikov A.V. ESTIMATION OF THE AVERAGE NUMBER OF EGGS IN LAYING OF LYMANTRIA DISPAR IN SAMARA REGION // Международный научно-исследовательский журнал 2016. — № 1(43). Pt. 2. — P. 109-111
• 6 Sedelnikov A.V., Molyavko D.P., Potienko K.I. Study of over-assessment of microaccelerations when using a beam-model of elastic elements // International Review of Aerospace Engineering 2016. — Vol. 9. Issue 1. — P. 7-12
• 7 Sedelnikov A.V., Potienko K.I. How to Estimate Microaccelerations for Spacecraft with Elliptical Orbit // Microgravity Science and Technology 2016. — Vol. 28. Issue 1. — P. 41-48

2017

• 1 Sedelnikov A.V., Potienko K.I. Analysis of reduction of controllability of spacecraft during conducting of active control over microaccelerations // International Review of Aerospace Engineering 2017. — Vol. 10. Issue 3. — P. 160-166
• 2 Sedelnikov A.V., Molyavko D.P., Potienko K.I. How Does Asymmetry of Solar Panels Influence Constructive Component of Microacceleration Field of Inner Environment of Space Laboratory // Microgravity Science and Technology 2017. — Vol. 29. Issue 4. — P. 305-311
• 3 Sedelnikov A.V., Potienko K.I. Application of Fractal Analysis While Designing of Family of Spacecraft for Needs of Space IndustryZagreb: InTech, 2017. 17p.
• 4 Sedel'nikov A. V., Khnyreva E. S. Формирование интегрального показателя нединамичности предприятия со слабой динамикой для эффективного управления им в кризисный период // Economics and Management 2017. — № 6 (140). — P. 36-42
• 5 Anshakov G.P., Belousov A. I. , Sedel’nikov A.V. The problem of estimating microaccelerations aboard Foton-M4 spacecraft // Russian Aeronautics 2017. — Vol. 60. Issue 1. — P. 83-89
• 6 Kozlovskiy V.N., Sedelnikov A.V., Khaimovich A.I. etc. Проблемы и перспективы развития системы мониторинга показателей качества автомобилей в эксплуатации // Известия Самарского научного центра РАН 2017. — Vol. 19. № 1. Pt. 1. — P. 31-39
• 7 Sedelnikov A.V. Evaluation of the level of microaccelerations on-board of a small satellite caused by a collision of a space debris particle with a solar panel // Jordan Journal of Mechanical and Industrial Engineering 2017. — Vol. 11. Issue 2. — P. 121-127

2018

• 1 Sedelnikov A., Khnyryova E., Ivashova T. A. Checking the correct operation of main measuring instruments on the flight model and prototype of AIST small spacecraft // MATEC Web of Conferences. — 2018. — Vol. 234.
• 2 Sedelnikov A.V., Filippov A.S., Gorozhakina A.S. Evaluation of calibration accuracy of magnetometer sensors of Aist small spacecraft // Journal of Physics: Conference Series. — 2018. — Vol. 1015. Issue 3.
• 3 Belousov A. I. , Sedelnikov A.V. Selecting the Parameters of the Orientation Engine for a Technological Spacecraft // IOP Conference Series: Materials Science and Engineering. — 2018. — Vol. 302. Issue 1.
• 4 Sedelnikov A.V. Fast analysis of onboard measurements of the earth magnetic field for the purpose of microaccelerations decrement on board of the “AIST” small spacecraft during its uncontrolled orbital flight // International Review of Aerospace Engineering 2018. — Vol. 11. Issue 2. — P. 76-83
• 5 Sedel'Nikov A.V., Safronov S.L., Filippov A.S. etc. Approach towards Establishing a Backup Satellite Attitude Control System Based on the Photovoltaic Array // MATEC Web of Conferences. — 2018. — Vol. 220.
• 6 Anshakov G.P., Belousov A. I. , Sedel’nikov A.V. etc. Efficiency Estimation of Electrothermal Thrusters Use in the Control System of the Technological Spacecraft Motion // Russian Aeronautics 2018. — Vol. 61. Issue 3. — P. 347-354
• 7 Sedelnikov A.V., Filippov A.S., Ivashova T. A. Earth's magnetic field measurements data accuracy evaluation on board of the small spacecraft "AIST" flight model // Jordan Journal of Mechanical and Industrial Engineering 2018. — Vol. 12. Issue 4. — P. 253-260
• 8 Sedelnikov A.V. Mean of Microaccelerations Estimate in the Small Spacecraft Internal Environment with the Use of Fuzzy Sets // Microgravity Science and Technology 2018. — Vol. 30. Issue 4. — P. 503-509

2019

• 1 Sedelnikov A.V., Safronov S.L., Khnyryova E.S. 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. — Vol. 1333. Issue 6.
• 2 Sedelnikov A.V., Rodina V.S., Orlov D. I. 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. — Vol. 1368. Issue 4.
• 3 Sedelnikov A.V., Safronov S.L., Khnyreva E.S. Control of rotational motion of a partially inoperable small spacecraft using fuzzy sets // Journal of Physics: Conference Series. — 2019. — Vol. 1260. Issue 3.
• 4 Belousov A. I. , Sedelnikov A.V., Gorozhakina A.S. The simulation results of the operation of a small spacecraft motion control system with an electrothermal microdrive // Journal of Physics: Conference Series. — 2019. — Vol. 1368. Issue 4.
• 5 Belousov A. I. , Sedelnikov A. Impact Analysis of Operation of Onboard Equipment on the Measurement Inaccuracies of Sensors // Proceedings - 2019 21st International Conference "Complex Systems: Control and Modeling Problems", CSCMP 2019. — 2019. — Vol. 2019-September. — P. 654-657
• 6 Anshakov G.P., Belousov A. I. , Sedel’nikov A.V. etc. Effect of the Mission and Supporting Equipment on Operation of the Magnetometer Sensors of the Foton-M No. 2 Spacecraft // Russian Aeronautics 2019. — Vol. 62. Issue 4. — P. 571-576
• 7 Sedelnikov A.V., Khnyryova E.S., Ivashova T. A. Some Features of a Small Spacecraft Application as a Technique for the World Ocean Exploration // IOP Conference Series: Earth and Environmental Science. — 2019. — Vol. 272. Issue 3.
• 8 Sedelnikov A.V., Khnyryova E.S., Filippov A.S. etc. Measurements analysis of the Earth's magnetic field data obtained from the flight model of AIST small spacecraft // International Journal of Mechanical Engineering and Robotics Research 2019. — Vol. 8. Issue 4. — P. 542-546
• 9 Anshakov G.P., Belousov A. I. , Sedelnikov A.V. etc. The micrometheroid influence estimate on the microaccelerations level onboard small spacecraft // Journal of Physics: Conference Series. — 2019. — Vol. 1210. Issue 1.

2020

• 1 Sedelnikov A., Filippov A., Khnyryova E. Test Results Analysis of Soft Hardware for Evaluating the Parameters of the Rotational Motion of a Small Spacecraft // 2020 International Multi-Conference on Industrial Engineering and Modern Technologies, FarEastCon 2020. — 2020. —
• 2 Sedelnikov A.V. 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. — Vol. 32. Issue 4. — P. 673-679
• 3 Sedelnikov A.V., Khnyryova E.S. Developing the Expert System for Assessing the Resilience to Crisis of Enterprises with Weak Dynamics // AEBMR-Advances in Economics Business and Management Research. — 2020. — Vol. 128. — P. 2612-2616
• 4 Sedelnikov A.V., Ivashova T. A. , Safronov S.L. 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. — Vol. 1441. Issue 1.
• 5 Sedelnikov A.V., Orlov D. I. 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. — Vol. 32. Issue 5. — P. 941-951
• 6 Sedelnikov A.V., Khnyryova E.S. 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. — Vol. 11. Issue 5.
• 7 Sedelnikov A.V. Accuracy assessment of microaccelerations simulation on the spacecraft “Foton-M” no. 2 according to magnetic measuring instruments data // Microgravity Science and Technology 2020. — Vol. 32. Issue 3. — P. 259-264

2021

• 1 Sedelnikov A.V. 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. — Vol. 14. Issue 8.
• 2 Sedelnikov A.V. Mathematical formalization of the process of crossing individuals of different populations within the framework of the quasispecies model // International Journal of Biomathematics 2021. — Vol. 14. Issue 4.
• 3 Sedelnikov A.V., Orlov D. I. 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. — Vol. 33. Issue 2.
• 4 Anshakov G.P., Belousov A. I. , Sedelnikov A.V. etc. Analysis of micro-acceleration requirements in the context of designing a small technological spacecraft // Journal of Physics: Conference Series. — 2021. — Vol. 1791. Issue 1.
• 5 Sedelnikov A.V., Orlov D. I. , Leskova Y.D. 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. — Vol. 1061. Issue 1.
• 6 Sedelnikov A.V., Serdakova V.V., Khnyryova E.S. 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. — Vol. 33. Issue 6.
• 7 Sedelnikov A.V., Taneeva A.S., Khnyryova E.S. etc. 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. — Vol. 1901. Issue 1.

2022

• 1 Sedelnikov A.V., Glushkov S.V., Serdakova V.V. etc. Simulating the stress-strain state of a thin plate after a thermal shock // International Journal of Modeling, Simulation, and Scientific Computing 2022. —
• 2 Sedelnikov A.V. Algorithm for Restoring Information of Current from Solar Panels of a Small Satellite Prototype "Aist" with Help of Normality Conditions // Journal of Aeronautics, Astronautics and Aviation 2022. — Vol. 54. Issue 1. — P. 67-76
• 3 Sedelnikov A.V. 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. —
• 4 Sedelnikov A., Orlov D.I., Khnyryova E. etc. Using the -Bdot Algorithm to Reduce the Angular Velocity of Rotation for the Aist Small Spacecraft Pilot Model // Advances in Transdisciplinary Engineering. — 2022. — Vol. 24. — P. 239-249
• 5 Sedelnikov A.V., Taneeva A.S. Dynamic characteristics modeling of rotary platform installed on board of a small spacecraft // OMFI-2021. — 2022. — Vol. 2182. Issue 1.
• 6 Sedelnikov A., Orlov D.I., Serdakova V.V. etc. Investigating the temperature field of large elastic elements of a small spacecraft for the Earth remote sensing to assess the effect of a temperature shock on its rotational motion // 2022 8th International Conference on Information Technology and Nanotechnology, ITNT 2022. — 2022. —
• 7 Sedelnikov A., Salmin V., Lazarev Y. etc. Compensating Microaccelerations from a Temperature Shock // Lecture Notes in Mechanical Engineering. — 2022. — P. 291-300
• 8 Sedelnikov A.V., Salmin V.V. Modeling the disturbing effect on the aist small spacecraft based on the measurements data // Scientific Reports 2022. — Vol. 12. Issue 1.
• 9 Sedelnikov A.V. Algorithm for Experimental Estimation of the Conditional Threshold for the Duration of Low Temperatures Exposure on the Example of the Laboratory-Reared Population of Lymanrtia Dispar // WSEAS Transactions on Biology and Biomedicine 2022. — Vol. 19. — P. 215-221
• 10 Sedelnikov A., Serdakova V.V., Orlov D.I. etc. Modeling the Effect of a Temperature Shock on the Rotational Motion of a Small Spacecraft, Considering the Possible Loss of Large Elastic Elements Stability // Microgravity Science and Technology 2022. — Vol. 34. Issue 4. № 4.
• 11 Sedelnikov A.V., Orlov D.I., Serdakova V.V. etc. Investigating the temperature field of large elastic elements of a small spacecraft for the Earth remote sensing to assess the effect of a temperature shock on its rotational motion // VIII Международная конференция и молодёжная школа «Информационные технологии и нанотехнологии» (ИТНТ-2022). — 2022. — Vol. 2.
• 12 Sedelnikov A.V., Serdakova V.V., Glushkov S.V. etc. 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. — Vol. 34. Issue 2.

2023

• 1 Sedelnikov A., Serdakova V.V., Nikolaeva A. etc. Numerical Simulation of the Stress-Strain State of a Thin Plate in the ANSYS Package as a Two-Dimensional Formulation of the Thermo-Elasticity // Applications of Modelling and Simulation 2023. — Vol. 7. — P. 156-167
• 2 Sedelnikov A., Orlov D.I., Serdakova V.V. etc. The Symmetric Formulation of the Temperature Shock Problem for a Small Spacecraft with Two Elastic Elements // Symmetry 2023. — Vol. 15. Issue 1. № 1.
• 3 Sedelnikov A.V., Orlov D.I., Serdakova V.V. etc. Investigation of the Stress-Strain State of a Rectangular Plate after a Temperature Shock // MATHEMATICS 2023. — Vol. 11. Issue 3. № 3.
• 4 Sedelnikov A., Orlov D.I., Serdakova V.V. etc. The importance of a three-dimensional formulation of the thermal conductivity problem in assessing the effect of a temperature shock on the rotational motion of a small spacecraft // E3S Web of Conferences. — 2023. — Vol. 371.
• 5 Sedelnikov A., Serdakova V.V., Nikolaeva A. Method of Taking into Account Influence of Thermal Shock on Dynamics of Small Satellite and its Use in Analysis of Microaccelerations // Microgravity Science and Technology 2023. — Vol. 35. Issue 3. № 3.
• 6 Sedelnikov A., Serdakova V.V., Orlov D.I. etc. Investigating the Temperature Shock of a Plate in the Framework of a Static Two-Dimensional Formulation of the Thermoelasticity Problem // Aerospace 2023. — Vol. 10. Issue 5. № 5.
• 7 Sedelnikov A.V., Taneeva A.S. Моделирование поля микроускорений в защищённой зоне виброзащитных устройств для реализации гравитационно-чувствительных процессов на борту малого космического аппарата технологического назначения // Омский научный вестник. Серия Авиационно-ракетное и энергетическое машиностроение 2023. — Vol. 7. № 2. — P. 65-72
• 8 Sedelnikov A.V., Orlov D.I., Bratkova M.E. etc. Estimating the Inertia Tensor Components of an Asymmetrical Spacecraft When Removing It from the Operational Orbit at the End of Its Active Life // Sensors (Switzerland) 2023. — Vol. 23. Issue 23. № 23.
• 9 Sedelnikov A.V., Eskina E.V., Taneeva A.S. etc. The problem of ensuring and controlling microaccelerations in the internal environment of a small technological spacecraft // Journal of Current Science and Technology 2023. — Vol. 13. Issue 1. № 1. — P. 1-11
• 10 Sedelnikov A.V., Bratkova M.E., Khnyryova E.S. Algorithm for the Operation of the Data-Measuring System for Evaluating the Inertial-Mass Characteristics of Space Debris // Lecture Notes in Electrical Engineering. — 2023. — Vol. 1047 LNEE. — P. 1087-1093

1996

• 1 Avramenko AA, Sedelnikov, AV Modeling a residual gravitation field on the board of orbital space device // IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA 1996. — Issue 4. — P. 22-25