Zabolotnov, Yuriy M.

2025

• 1 Zhang Y., Wang C., Zabolotnov Y. etc. Analysis of satellite attitude motion in a three-body tethered system during deployment via integral manifolds // Acta Astronautica 2025. — Vol. 226. — P. 716-727

2014

• 1 Zabolotnov Yu. , Kang J., Wang W. etc. Smooth Tension Control Strategy for Space Tether Deployment // Computer Simulation 2014. — № 3. — P. 83-86
• 2 Zabolotnov Yu. , Dong Ch., Li Ai. etc. Modeling and Simulation Analysis Equilibrium Position of Space Tether System // J. Computer Simulation 2014. — № 2. — P. 160-164
• 3 Li Ch., Wang W., Li Ai. etc. Control for Station-Keeping Phase of Based of Standard Coefficient Method // // J. Aerospace Control 2014. — № Vol.32. No.2. — P. 73-77
• 4 Li A., Wei H., Wang C. etc. Calculating reentry conditions for space tether-assisted return system // Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 2014. — Vol. 32. Issue 5. — P. 730-736
• 5 Wang C., Zhang M., Li A. etc. Dynamics modeling and trajectory tracking control of space tether system // Yingyong Lixue Xuebao/Chinese Journal of Applied Mechanics 2014. — Vol. 31. Issue 6. — P. 895-899
• 6 Wang Ch., Zhang M., Wang W. etc. Optimal control state keeping stage of tethered satellite with random perturbation // Chinese J. of Space Science 2014. — № Vol. 34. No.6. — P. 881-886
• 7 Zabolotnov Yu.M., Lobankov A.A. Аналитический метод расчета регулятора для колебательной системы с двумя степенями свободы // Известия Самарского научного центра РАН 2014. — Vol. 16. № 4 (2). — P. 432-435
• 8 Zabolotnov Y.M., Elenev D.V. A way for accelerated calculation of spacecraft motion in an atmosphere with a tethered aerodynamic stabilizer // Mathematical Models and Computer Simulations 2014. — Vol. 6. Issue 1. — P. 38-45

1984

• 1 Belokonov V.M., Belokonov I.V., Zabolotnov Yu.M. FAST SIMULATION METHOD FOR QUASI-PERIODIC MOTION OF AN ALMOST AXISYMMETRIC RIGID BODY IN THE ATMOSPHERE. // Mechanics of Solids 1984. — Vol. 19. Issue 2. — P. 41-48

1990

• 1 Zabolotnov Yu.M. An asymptotic method for quasilinear vibrational systems with an aperiodic generating solution // USSR Computational Mathematics and Mathematical Physics 1990. — Vol. 30. Issue 2. — P. 46-56

1998

• 1 Zabolotnov Yu.M., Lyubimov V.V. Secondary resonance effect in the motion of a spacecraft in the atmosphere // Cosmic Research 1998. — Vol. 36. Issue 2. — P. 194-201

2002

• 1 Zabolotnov Y.M., Lyubimov V.V. Non-linear resonance evolutionary effects in the motion of a rigid body about a fixed point // Journal of Applied Mathematics and Mechanics 2002. — Vol. 66. Issue 3. — P. 401-408
• 2 Zabolotnov Yu.M., Lyubimov V.V. Non-linear resonance evolutionary effects in the motion of a rigid body about a fixed point // Prikladnaya Matematika i Mekhanika 2002. — Vol. 66. Issue 3. — P. 410-417

2003

• 1 Zabolotnov Yu.M., Lyubimov V.V. Application of the method of integral manifolds for construction of resonant curves for the problem of spacecraft entry into the atmosphere // Cosmic Research 2003. — Vol. 41. Issue 5. — P. 453-459

2010

• 1 Zabolotnov Y.M., Nikonova I.A. Disturbance ranging in capsule atmosphere descent // Russian Aeronautics 2010. — Vol. 53. Issue 4. — P. 375-381

2012

• 1 Zabolotnov Y.M., Naumov O. N. Motion of a descent capsule relative to its center of mass when deploying the orbital tether system // Cosmic Research 2012. — Vol. 50. Issue 2. — P. 177-187

2013

• 1 ZABOLOTNOV Yu.M. Introduction of Space tether system motion dynamics and control (Russia) (Введение в динамику и управление движением космических тросовых систем)Пекин: Beijing: Science Press, 2013. 140p.
• 2 Zabolotnov Y.M. Statistical analysis of attitude motion of a light capsule entering the atmosphere // Cosmic Research 2013. — Vol. 51. Issue 3. — P. 213-224
• 3 Zabolotnov Y.M., Elenev D.V. Stability of motion of two rigid bodies connected by a cable in the atmosphere // Mechanics of Solids 2013. — Vol. 48. Issue 2. — P. 156-164

2015

• 1 Zabolotnov Yu.M., Lobankov A.A. Оптимальное демпфирование колебаний твердого тела при его движении вокруг неподвижной точки // Известия Самарского научного центра РАН 2015. — Vol. 17. № 2 (5). — P. 970-973
• 2 Zabolotnov Y.M. Control of the deployment of a tethered orbital system with a small load into a vertical position // Journal of Applied Mathematics and Mechanics 2015. — Vol. 79. Issue 1. — P. 28-34

2024

• 1 Wang L., Li A., Wang C. etc. ROBUST SLIDING MODE CONTROL FOR UAV FORMATION WITH EXTERNAL DISTURBANCES UNDER EVENT-TRIGGERED STRATEGY // ICAS Proceedings. — 2024. —
• 2 Zhang Y., Wang C., Zabolotnov Y. etc. Attitude Control of End Satellites in the Three-body Tethered System Based on the Averaging Method; [基于平均方法的三体绳系系统末端星体姿态控制] // Yuhang Xuebao/Journal of Astronautics 2024. — Vol. 45. Issue 8. № 8. — P. 1261-1268
• 3 Wang L., Li A., Lu H. etc. Distributed adaptive event-triggered finite-time fault-tolerant containment control for multi-UAVs with input constraints and actuator failures // Journal of the Franklin Institute 2024. — Vol. 361. Issue 18. № 18.
• 4 Li L., Li A., Lu H. etc. Collision-avoidance strategy for a spinning electrodynamic tether system // Astrodynamics 2024. — Vol. 8. Issue 2. № 2. — P. 247-259
• 5 Wang L., Li A., Xiao C. etc. Distributed adaptive disturbance observer-based multi-channel event-triggered finite-time coordinated control for multi-UAVs with actuator failures // Aerospace Science and Technology 2024. — Vol. 151.
• 6 Zabolotnov Y.M., Wang C., Min Z. Control of the Process of Rapprochement of a Tether System with a Passive Space Object in a Near-Circular Orbit // Cosmic Research 2024. — Vol. 62. Issue 3. № 3. — P. 276-285
• 7 Lu H., Wang C., Li A. etc. Sliding Mode Control Strategy of Spinning Electrodynamic Tether Formation during Its Spin-Up Process // IEEE Transactions on Aerospace and Electronic Systems 2024. — Vol. 60. Issue 1. № 1. — P. 449-462

2016

• 1 Zabolotnov Y.M. The resonance motions of a statically stable Lagrange top at small nutation angles // Journal of Applied Mathematics and Mechanics 2016. — Vol. 80. Issue 4. — P. 302-310
• 2 Zabolotnov Y.M. Application of the integral manifold method to the analysis of the spatial motion of a rigid body fixed to a cable // Mechanics of Solids 2016. — Vol. 51. Issue 4. — P. 371-384
• 3 Wang C.-Q., Wei H.-L., Li A.-J. etc. Sliding mode variable structure control for the deployment of tethered satellite system // Kongzhi Lilun Yu Yingyong/Control Theory and Applications 2016. — Vol. 33. Issue 1. — P. 70-76
• 4 Shi L.H., Changqing W., Yuriy Z. etc. Optimal Control of Payload Tossing Using Space Tethered System // IFAC-PapersOnLine 2016. — Vol. 49. Issue 17. — P. 272-277
• 5 Dong Z., Zabolotnov Y.M., Wang C.Q. CONTROL OF SPACE TETHER SYSTEM DEPLOYMENT WITH ATMOSPHERIC PROBE // Перспективные информационные технологии (ПИТ 2016). — 2016. — P. 3-6
• 6 Zabolotnov Y.M., Don Ch., Van Ch. Анализ динамики развертываемой космической тросовой системы с атмосферным зондом // Известия Самарского научного центра РАН 2016. — Vol. 18. № 4(4). — P. 726-732

2017

• 1 Zabolotnov Y.M., Lobanov A.A. Synthesis of a controller for stabilizing the motion of a rigid body about a fixed point // Mechanics of Solids 2017. — Vol. 52. Issue 3. — P. 278-288
• 2 Elenev D.V., Zabolotnov Y.M. Analysis of the dynamics of the deployed aerodynamic space tether system // Cosmic Research 2017. — Vol. 55. Issue 5. — P. 371-379
• 3 Zabolotnov Yu.M. Dynamics of the Formation of a Rotating Orbital Tether System with the Help of Electro-thruster // Procedia Engineering. — 2017. — Vol. 185. — P. 261-266
• 4 Zabolotnov Y.M. Control of the deployment of an orbital tether system that consists of two small spacecraft // Cosmic Research 2017. — Vol. 55. Issue 3. — P. 224-233
• 5 Van Ch., Zabolotnov Yu.M. Управление при развертывании тросовой системы на эллиптической орбите // Известия Самарского научного центра РАН 2017. — Vol. 19. Issue 1. № 1. — P. 91-97
• 6 Dong Z., Zabolotnov Y.M., Wang C. Modeling and analysis of deployment dynamics of a distributed orbital tether system with an atmospheric sounder // Advances in the Astronautical Sciences. — 2017. — Vol. 161. — P. 1051-1061
• 7 Elenev D.V., Zabolotnov Y.M., McMillan A.J. Deployment and stabilization of an aerodynamic space tether system // Advances in the Astronautical Sciences. — 2017. — Vol. 161. — P. 1023-1030
• 8 Zabolotnov Yu.M., Lyubimov V.V., Kurkina E.V. Evaluation of Asymmetric Small Satellite with Electric Propulsion Perturbations when Passing through Resonance // Procedia Engineering. — 2017. — Vol. 185. — P. 299-303
• 9 Zabolotnov Y.M., Elenev D.V. Deployment of an orbital tethered system with an aerodynamic stabilizer // Mechanics of Solids 2017. — Vol. 52. Issue 1.
• 10 Elenev D., Zabolotnov Y. Modeling and analysis of motion of a spacecraft with a tether aerodynamic stabilizer // CEUR Workshop Proceedings. — 2017. — Vol. 1904. — P. 85-88
• 11 Van Chancin , Zabolotnov YU.M. Управление развёртыванием орбитальной тросовой системы большой протяжённости // Vestnik of Samara University. Aerospace and Mechanical Engineering 2017. — Vol. 16. № 2. — P. 7-17

2018

• 1 Wang C.Q., Zabolotnov Y.M. Modeling and analysis of the process of forming a vertical tether group of nano-satellites // Journal of Physics: Conference Series. — 2018. — Vol. 1096. Issue 1.
• 2 Lu Kh. , Aijun L., Changqing W. etc. Impact analysis and adaptive sliding mode control for cislunar payload transportation using spinning tether system // Aircraft Engineering and Aerospace Technology 2018. — Vol. 90. Issue 8. — P. 1168-1179
• 3 Dong Z., Zabolotnov Y.M., Wang C. Motion modeling and deployment control of a long tethered spacecraft system with an atmospheric sounder // Engineering Letters 2018. — Vol. 26. Issue 4. — P. 478-488
• 4 Dong Z., Zabolotnov Y.M., Li A.J. etc. Mathematical modeling and analysis of motion of a low-orbital space tether system // Journal of Physics: Conference Series. — 2018. — Vol. 1096. Issue 1.

2019

• 1 Voevodin P.S., Zabolotnov Y.M. Stabilizing the Motion of a Low-Orbit Electrodynamic Tether System // Journal of Computer and Systems Sciences International 2019. — Vol. 58. Issue 2. — P. 270-285
• 2 Lu Kh. , Zabolotnov Y.M., Li A. Application of spinning electrodynamic tether system in changing system orbital parameters // Journal of Physics: Conference Series. — 2019. — Vol. 1368. Issue 4.
• 3 Zhe D., Zabolotnov Y.M., Haiquan W. etc. Modeling and Analysis of Deployment Dynamics of a Low-orbital Tethered System // International Conference on Advanced Mechatronic Systems, ICAMechS. — 2019. — Vol. 2019-August. — P. 353-358
• 4 Voevodin P., Zabolotnov Y. Simulation of the Braking Process of a Nanosatellite Using an Electrodynamic Tether System // Proceedings - 2019 21st International Conference "Complex Systems: Control and Modeling Problems", CSCMP 2019. — 2019. — Vol. 2019-September. — P. 634-639
• 5 Voevodin P.S., Zabolotnov Y.M. On Stability of the Motion of Electrodynamic Tether System in Orbit Near the Earth // Mechanics of Solids 2019. — Vol. 54. Issue 6. — P. 890-902
• 6 Zabolotnov Y.M. Resonant Motions of the Statically Stable Lagrange Spinning Top // MECHANICS OF SOLIDS 2019. — Vol. 54. Issue 5. № 5. — P. 652-668
• 7 Wang C., Fu L., Zabolotnov Y. etc. Matrix decomposition based control for space tether system with incomplete state feedback // Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics 2019. — Vol. 45. Issue 5. — P. 902-911
• 8 Dong Z., Zabolotnov Y.M., Li A.J. etc. Modeling and comparative analysis of schemes for returning a payload using a space tethered system // Journal of Physics: Conference Series. — 2019. — Vol. 1368. Issue 4.

2020

• 1 Lu Kh. , Li A., Wang C. etc. Stability analysis and motion control of spinning electrodynamic tether system during transition into spin // Acta Astronautica 2020. — Vol. 177. — P. 871-881
• 2 Lu Kh. , Zabolotnov Y., Li A. Impact analysis and orbit reboost of payload tossing using spinning electrodynamic tether system // International Journal of Engineering Systems Modelling and Simulation 2020. — Vol. 11. Issue 4. — P. 176-185
• 3 Voevodin P.S., Zabolotnov Y.M. Analysis of the Dynamics and Choice of Parameters of an Electrodynamic Space Tether System in the Thrust Generation Mode // Cosmic Research 2020. — Vol. 58. Issue 1. — P. 42-52
• 4 Zabolotnov Y., Ledkova T. A. Modelling and analysis of the motion of a space tether system in a lunar orbit // Proceedings of ITNT 2020 - 6th IEEE International Conference on Information Technology and Nanotechnology. — 2020. —
• 5 Zabolotnov Yu.M. Approximate optimal method for controlling the angular motion of a spacecraft as part of an orbital tether system // IOP Conference Series: Materials Science and Engineering. — 2020. — Vol. 984. Issue 1.
• 6 Chen S., Wang C., Yuriy Z. etc. Attitude dynamic analysis of the end-bodies of space tether system in deployment // Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology 2020. — Vol. 42. Issue 2. — P. 98-106

2021

• 1 Zabolotnov Y.M. Resonance Effects when Moving a Small Spacecraft around the Center of Mass in a Deployable Tether System // Cosmic Research 2021. — Vol. 59. Issue 4. — P. 291-304
• 2 Wang C., Zabolotnov Y.M. Analysis of the Dynamics of the Formation of a Tether Group of Three Nanosatellites Taking into Account Their Motion around the Centers of Mass // Mechanics of Solids 2021. — Vol. 56. Issue 7. — P. 1181-1198
• 3 Lu H., Li A., Wang C. etc. Tether Deformation of Spinning Electrodynamic Tether System and Its Suppression with Optimal Controller // JOURNAL OF AEROSPACE ENGINEERING 2021. — Vol. 34. Issue 2. № 2.

2022

• 1 Zabolotnov Y.M., Nazarova A.A. Method of Forming a Triangular Rotating Tethered Constellation of Spacecraft Using Electromagnetic Forces // Journal of Computer and Systems Sciences International 2022. — Vol. 61. Issue 4. № 4. — P. 677-692
• 2 Voevodin P.S., Zabolotnov Y.M. Quasi-Optimal Stabilization of Oscillatory Systems with Many Degrees of Freedom // Journal of Computer and Systems Sciences International 2022. — Vol. 61. Issue 3. — P. 332-347
• 3 Zabolotnov Y.M., Nazarova A.A., Wang C. etc. The Dynamics of Arranging a Spacecraft Tether Group as a Triangular Constellation // Cosmic Research 2022. — Vol. 60. Issue 5. № 5. — P. 375-386
• 4 Zabolotnov Y.M., Voevodin P.S., Hongshi L. A TWO-STAGE METHOD FOR THE FORMATION OF A ROTATING ELECTRODYNAMIC SPACE TETHER SYSTEM // Mechanics of Solids 2022. — Vol. 57. Issue 3. № 3. — P. 462-475
• 5 Ben W., Changqing W., Aijun L. etc. Robust Sliding Mode Tracking Control for Linear Tethered Satellite Formation Deployment // Lecture Notes in Electrical Engineering. — 2022. — Vol. 644 LNEE. — P. 3435-3447
• 6 Peijie S., Changqing W., Zabolotnov Y.M. etc. Design of Space Transit Transportation Task Based on Nonsingular Finite-Time Control // Lecture Notes in Electrical Engineering. — 2022. — Vol. 644 LNEE. — P. 2715-2726
• 7 Qiang F., Changqing W., Aijun L. etc. The Space Tether System Deorbit Control with Parameter Optimization // Lecture Notes in Electrical Engineering. — 2022. — Vol. 644 LNEE. — P. 2677-2688

2023

• 1 Zabolotnov Y.M., Nazarova A.A., Wang C. Analysis of Dynamics and Control During the Deployment of an Annular Tether Group of Spacecraft // Mechanics of Solids 2023. —
• 2 Lu Kh., Li A., Wang C. etc. Impact Stabilization of Spinning Tether Systems After Nonideal Rendezvous // JOURNAL OF SPACECRAFT AND ROCKETS 2023. — Vol. 60. Issue 1. № 1. — P. 59-67
• 3 Chen Sh., Liu C., Zabolotnov Yu.M. etc. Stable Deployment Control of a Multi-tethered Formation System Considering the Spinning Motion of Parent Satellite // Lecture Notes in Electrical Engineering. — 2023. — Vol. 913. — P. 771-782
• 4 Zabolotnov Y.M. Approximately Optimal Stabilization of a Gyroscopic System with Many Degrees of Freedom and Slowly Varying Parameters // Gyroscopy and Navigation 2023. — Vol. 14. Issue 1. № 1. — P. 89-95
• 5 Chen S., Zabolotnov Y.M. Method of Forming a Regular Triangular Tethered Constellation of Microsatellites with Considering Their Motion Relative to the Centers of Mass // Journal of Computer and Systems Sciences International 2023. — Vol. 62. Issue 1. № 1. — P. 27-42

1983

• 1 Belokonov V.M., Belokonov I.V., Zabolotnov Yu.M. ACCELERATED CALCULATION OF THE DESCENT TRAJECTORY IN THE ATMOSPHERE OF UNGUIDED SPACECRAFT TAKING INTO ACCOUNT THEIR MOTION RELATIVE TO THE CENTER OF MASS. // Cosmic Research 1983. — Vol. 21. Issue 4. — P. 415-423