Dr. Levskii Mikhail Valerevich

Research Scientist
Russian Space Research Institute, Russia

Highest Degree
Ph.D. in Engineering Science from Russian Space Research Institute, Russia

My URL
https://livedna.org/712.25010

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Area of Interest:

Engineering
Automation and Control
Space Robotics
Space Structure
Spectroscopy

Selected Publications

  1. Levskii, M.V., 2019. Restricted quadratic optimal control of a spacecraft turning in a fixed time period. J. Comput. Syst. Sci. Int., 58: 126-146.
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  2. Levskii, M.V., 2018. Special mode for increasing the efficiency of spaccraft's motion control. Int. J. Comput. Appl. Telecommun., 1: 1-15.

  3. Levskii, M.V., 2018. Reconstruction of functions which describe motion of rigid body under measurements using the method of trained models. Int. J. Math. Anal. Applic., 5: 15-23.

  4. Levskii, M.V., 2018. Quadratic optimal control in reorienting a spacecraft in a fixed time period in a dynamic problem statement. J. Comput. Syst. Sci. Int., 57: 131-148.

  5. Levskii, M.V., 2018. Optimization of spatial rotations of the spacecraft controlled by inertial actuators. Am. J. Math. Comput. Sci., 3: 22-30.

  6. Levskii, M.V., 2018. High-effective method of economical control of spacecraft motion with long life on orbit. Am. J. Math. Comput. Sci., 3: 41-49.

  7. Levskii, M.V., 2018. Analytic controlling reorientation of a spacecraft using a combined criterion of optimality. J. Comput. Syst. Sci. Int., 57: 283-301.
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  8. Levskii, M.V., 2017. The case of optimal control with exceptional role of the conditions of transversality. Int. Robotics Automat. J., Vol. 3. 10.15406/iratj.2017.03.00055.
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  9. Levskii, M.V., 2017. Special aspects in attitude control of a spacecraft, equipped with inertial actuators. J. Comput. Sci. Applic. Inform. Technol., 2: 1-9.

  10. Levskii, M.V., 2016. To problem of turn optimality for the spacecraft with power-gyroscopes. Actual Problems Aviation Aerospace Syst.: Processes Models Exp., 21: 134-144.

  11. Levskii, M.V., 2016. On the problem of optimal spacecraft attitude control. J. Comput. Syst. Sci. Int., 55: 310-330.
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  12. Levskii, M.V., 2016. About transversality conditions for solving variation problems. Int. IFNA-ANS J. Probl. Nonl. Anal. Eng. Syst., 22: 114-123.

  13. Levskii, M.V., 2015. Kinematically optimal spacecraft attitude control. J. Comput. Syst. Sci. Int., 54: 116-132.
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  14. Levskii, M.V., 2015. About method for solving the optimal control problems of spacecraft spatial orientation. Int. IFNA-ANS J. Probl. Nonl. Anal. Eng. Syst., 21: 61-75.
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  15. Levskiy, M.V., 2014. The time-optimal control of motion of a spacecraft with inertial executive devices. Int. Russian-Am. Scient. J. Actual Problems Aviation Aerospace Syst., 19: 88 -98.

  16. Levskiy, M.V., 2014. An investigation of spatial turn regime of multimodular space station. Int. Russian-Am. Scient. J. Actual Problems Aviation Aerospace Syst., 19: 33-44.

  17. Levskii, M.V., 2012. A special case of spacecraft optimal attitude control. J. Comput. Syst. Sci. Int., 51: 587-601.
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  18. Levskii, M.V., 2011. Some issues of time-optimal control over a spacecraft programmed turn. Cosmic Res., 49: 521-533.
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  19. Levskii, M.V., 2011. Optimal control of reorientation of a spacecraft using free trajectory method. Cosmic Res., 49: 131-149.
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  20. Levskii, M.V., 2011. On optimal spacecraft damping. J. Comput. Syst. Sci. Int., 50: 144-157.
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  21. Levskii, M.V., 2010. Controlling space vehicle reorientation with minimal energy itegral. Autom. Remote Control, 71: 2518-2533.
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  22. Levskii, M.V., 2009. Use of the energy integral in optimal control of the spacecraft spatial attitude. Mech. Solids, 44: 502-513.
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  23. Levskii, M.V., 2009. The problem of the time-optimal control of spacecraft reorietation. J. Applied Math. Mech., 73: 16-25.
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  24. Levskii, M.V., 2009. Optimal spacecraft terminal attitude control synthesis by the quaternion method. Mech. Solids, 44: 169-183.
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  25. Levskii, M.V., 2008. Pontryagin’s maximum principle in optimal control problems of orientation of a spacecraft. J. Comput. Syst. Sci. Int., 47: 974-986.
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  26. Levskii, M.V., 2007. Control of spatial reorientation of a space craft using the free trajectory method. J. Comput. Syst. Sci. Int., 46: 962-975.
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  27. Levskii, M.V., 2007. Control of a spacecraft’s spatial turn with minimum value of the path functional. Cosmic Res., 45: 234-247.
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  28. Levskii, M.V., 2004. Optimal control of a spatial turn of a spacecraft with minimal loading of construction. Cosmic Res., 42: 414-426.
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  29. Levskii, M.V., 2003. Optimal control of a programmed turn of a spacecraft. Cosmic Res., 41: 178-192.
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  30. Levskii, M.V., 2002. Optimization problem in control over a programmed turn of a spaccraft. Cosmic Res., 40: 479-489.
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  31. Levskii, M.V., 1999. Solution to the problem of optimum control of a programmed spac craft turn with the use of a predicting model. Cosmic Res., 37: 220-220.
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  32. Levskii, M.V., 1998. Optimal control of spacecraft reorientation combined with orbit correction. Cosmic Res., 36: 178-187.
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  33. Levskii, M.V., 1997. Solution of a problem of optimal control of the programmed turn of a spacecraft using prognostic models. Cosmic Res., 35: 278-283.
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  34. Levskii, M.V., 1996. On finding the optimal parameters of spacecraft spin-up. Cosmic Res., 34: 602-608.
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  35. Levskii, M.V., 1995. Optimal control of the spatial turn of a spacecraft. Cosmic Res., 33: 452-456.
Member since September, 2018