Ishkov, Sergey A.

2024

• 1 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

2023

• 1 Ishkov S.A., Filippov G.A., Zhou X. etc. Pareto⁃optimal control of relative motion in the orbital maneuvering problem of spacecraft with finite thrust; [帕累托 -有限推力航天器轨道机动问题中相对运动的最优控制] // Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 2023. — Vol. 41. Issue 3. № 3. — P. 529-536
• 2 Ishkov S.A., Filippov G.A. Research for Optimal Programs for Controlling the Relative Motion of a Spacecraft with Limited Thrust // Cosmic Research 2023. — Vol. 61. Issue 3. № 3. — P. 249-257

2021

• 1 Fadeenkov P.V., Ishkov S.A. Selection motion control programs of spacecraft with low thrust for supporting nearly-circular orbit // Advances in the Astronautical Sciences. — 2021. — Vol. 174. — P. 129-134

2020

• 1 ELISOV N.A., ISHKOV S.A., LOMAKA I.A. etc. Influence of non-equilibrium reactions on the optimization of aerothrust aeroassisted maneuver with orbital change // Chinese Journal of Aeronautics 2020. — Vol. 33. Issue 8. — P. 2133-2145

2019

• 1 Fadeenkov P., Ishkov S. Low thrust spacecraft motion control with simultaneous changes in main orbital elements // Mathematics in Engineering, Science and Aerospace 2019. — Vol. 10. Issue 4. — P. 733-738
• 2 Balakin V. L. , Elisov N., Ishkov S. etc. Comparative analysis of principle maximum and differential evolution in the problem of the combined orbital plane rotation maneuver // Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019. — 2019. — P. 131-136
• 3 Ishkov S., Balakin V. L. , Khramov A. A. etc. Optimizing an ascent trajectory of a small spacecraft launched by an air-based two-stage rocket // Proceedings of 9th International Conference on Recent Advances in Space Technologies, RAST 2019. — 2019. — P. 181-185

2018

• 1 Elisov N.A., Ishkov S.A., Shakhov V. G. Numerical analysis of air dissociation influence on spaceplane aerodynamic characteristics // Acta Astronautica 2018. — Vol. 148. — P. 153-162
• 2 Ishkov S.A., Filippov G. A. , Fadeenkov P.V. Nominal control program in problem of far rendezvous at geostationary orbit with low transversal thrust // AIP Conference Proceedings. — 2018. — Vol. 2046.
• 3 Ishkov S.A., Filippov G. A. , Kremeneckaya M.E. etc. Ballistic analyze of spacecraft inspector motion, equipped with electric thruster, above International Space Station // AIP Conference Proceedings. — 2018. — Vol. 2046.
• 4 Ishkov S.A., Filippov Grigoriy Aleksandrovich, Fadeenkov P.V. Оптимальные программы управления по быстродействию в задаче сближения с малой трансверсальной тягой // Vestnik of Samara University. Aerospace and Mechanical Engineering 2018. — Vol. 17. № 4. — P. 67-80
• 5 Balakin V.L., Ishkov S.A., Khramov A.A. Оптимизация комбинированного поворота плоскости орбиты аэрокосмического аппарата на основе метода последовательной линеаризации // Vestnik of Samara University. Aerospace and Mechanical Engineering 2018. — Vol. 17. № 2. — P. 23-36
• 6 Elisov N.A., Ishkov S.A., Shakhov V. G. The aerodynamic characteristics of the payload set-upped out of aircraft // AIP Conference Proceedings. — 2018. — Vol. 2046.
• 7 Balakin V.L., Ishkov S. A., Khramov A.A. Оптимизация трансатмосферного движения летательного аппарата на основе метода принципа максимума Понтрягина // Vestnik of Samara University. Aerospace and Mechanical Engineering 2018. — Vol. 17. № 1. — P. 7-19
• 8 Balakin V. L. , Elisov N.A., Ishkov S.A. etc. Evaluation of the spaceplane maneuverability during combined orbital plane changes // AIP Conference Proceedings. — 2018. — Vol. 2046.
• 9 Fadeenkov P.V., Ishkov S.A. Optimum program of control of continuous low-thrust at flight between noncoplanar elliptical and geostationary orbits // AIP Conference Proceedings. — 2018. — Vol. 2046.
• 10 Ishkov S.A., Khramov A. A. , Filippov G. A. Formation algorithms of sequential control for spacecraft rendezvous with low-thrust // AIP Conference Proceedings. — 2018. — Vol. 2046.

2017

• 1 Ishkov S.A., Petrukhina K.V., Salmin V.V. Calculating Launch Windows for Transfers of Solar Powered EP Spacecraft between Low-earth Non-coplanar Circular Orbits // Procedia Engineering. — 2017. — Vol. 185. — P. 338-344
• 2 Ishkov S.A., Filippov G. A. Special Refill Spacecraft Debris Collector, Equipped with Electro Rocket Engine of Low-thrust, Design Parameters Optimization // Procedia Engineering. — 2017. — Vol. 185. — P. 396-403
• 3 Ishkov S.A., Filippov G. A. , Khramov A. A. Autonomous Control Program for Special Spacecraft Debris Collector Rendezvous Transfer with Fragment of Space Debris with Low-thrust // Procedia Engineering. — 2017. — Vol. 185. — P. 388-395
• 4 Ishkov S.A. Optimization of Design Parameters of Spacecraft Equipped with Electro Rocket Low-thrust Engine and Calculation its Applying Area at Low Earth Orbit // Procedia Engineering. — 2017. — Vol. 185. — P. 239-245
• 5 Ishkov S.A., Khramov A. A. Evaluation of the Efficiency of Propulsion Systems Usage with Energy Accumulation at Spacecraft // Procedia Engineering. — 2017. — Vol. 185. — P. 212-219
• 6 Balakin V.L., Ishkov S. A., Khramov A.A. Оптимизация трансатмосферного движения летательного аппарата на основе метода последовательной линеаризации // Vestnik of Samara University. Aerospace and Mechanical Engineering 2017. — Vol. 16. № 3. — P. 17-26

2016

• 1 Khramov A. A. , Ishkov S.A. Optimization of project-ballistic parameters for low earth orbit spacecraft with propulsion systems with energy storage // Russian Aeronautics 2016. — Vol. 59. Issue 3. — P. 351-357
• 2 Ishkov S.A., Filippov G.A., Khramov A.A. Номинальная программа управления сближением космического аппарата – сборщика мусора с электроракетным двигателем малой тяги на геостационарной орбите // Известия Самарского научного центра РАН 2016. — Vol. 18. № 4 (6). — P. 1215-1222
• 3 Xu X., Ishkov S.A., Faddeenkov P.V. etc. Analyzing deviations of returning load from targeted landing point when space tether system is used // Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University 2016. — Vol. 34. Issue 2. — P. 294-298

2015

• 1 Ishkov S.A., Filippov G. A. A disposal of the space debris with special spacecraft debris collector using low trust // Engineering Letters 2015. — Vol. 23. Issue 2. — P. 98-109

1997

• 1 Ishkov S.A. Calculation of optimal transfers with low transversal thrust into an elliptical orbit // Cosmic Research 1997. — Vol. 35. Issue 2. — P. 166-175
• 2 Ishkov S.A., Romanenko V.A. Forming and correction of a high-elliptical orbit of an Earth satellite with low-thrust engine // Cosmic Research 1997. — Vol. 35. Issue 3. — P. 268-277

1984

• 1 Ishkov S.A., Salmin V.V. OPTIMAL CONTROL PROGRAMS IN THE PROBLEM OF TRANSFER FLIGHT BETWEEN ORBITS WITH CONTINUOUS THRUST. // Cosmic Research 1984. — Vol. 22. Issue 5. — P. 569-578