Dr. Levskii Mikhail Valerevich
My Social Links

Dr. Levskii Mikhail Valerevich

Research Scientist
Russian Space Research Institute, Russia

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

Share this Profile

Area of Interest:

Engineering
100%
Automation and Control
62%
Space Robotics
90%
Space Structure
75%
Spectroscopy
55%

Research Publications in Numbers

Books
0
Chapters
0
Articles
35
Abstracts
0

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.
    CrossRef  |  Direct Link  |  
  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.
    CrossRef  |  Direct Link  |  
  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.
    CrossRef  |  Direct Link  |  
  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.
    CrossRef  |  Direct Link  |  
  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.
    CrossRef  |  Direct Link  |  
  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.
    Direct Link  |  
  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.
    CrossRef  |  Direct Link  |  
  18. Levskii, M.V., 2011. Some issues of time-optimal control over a spacecraft programmed turn. Cosmic Res., 49: 521-533.
    CrossRef  |  Direct Link  |  
  19. Levskii, M.V., 2011. Optimal control of reorientation of a spacecraft using free trajectory method. Cosmic Res., 49: 131-149.
    CrossRef  |  Direct Link  |  
  20. Levskii, M.V., 2011. On optimal spacecraft damping. J. Comput. Syst. Sci. Int., 50: 144-157.
    CrossRef  |  Direct Link  |  
  21. Levskii, M.V., 2010. Controlling space vehicle reorientation with minimal energy itegral. Autom. Remote Control, 71: 2518-2533.
    CrossRef  |  Direct Link  |  
  22. Levskii, M.V., 2009. Use of the energy integral in optimal control of the spacecraft spatial attitude. Mech. Solids, 44: 502-513.
    CrossRef  |  Direct Link  |  
  23. Levskii, M.V., 2009. The problem of the time-optimal control of spacecraft reorietation. J. Applied Math. Mech., 73: 16-25.
    CrossRef  |  Direct Link  |  
  24. Levskii, M.V., 2009. Optimal spacecraft terminal attitude control synthesis by the quaternion method. Mech. Solids, 44: 169-183.
    CrossRef  |  Direct Link  |  
  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.
    CrossRef  |  Direct Link  |  
  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.
    CrossRef  |  Direct Link  |  
  27. Levskii, M.V., 2007. Control of a spacecraft’s spatial turn with minimum value of the path functional. Cosmic Res., 45: 234-247.
    CrossRef  |  Direct Link  |  
  28. Levskii, M.V., 2004. Optimal control of a spatial turn of a spacecraft with minimal loading of construction. Cosmic Res., 42: 414-426.
    CrossRef  |  Direct Link  |  
  29. Levskii, M.V., 2003. Optimal control of a programmed turn of a spacecraft. Cosmic Res., 41: 178-192.
    CrossRef  |  Direct Link  |  
  30. Levskii, M.V., 2002. Optimization problem in control over a programmed turn of a spaccraft. Cosmic Res., 40: 479-489.
    CrossRef  |  Direct Link  |  
  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.
    Direct Link  |  
  32. Levskii, M.V., 1998. Optimal control of spacecraft reorientation combined with orbit correction. Cosmic Res., 36: 178-187.
    Direct Link  |  
  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.
    Direct Link  |  
  34. Levskii, M.V., 1996. On finding the optimal parameters of spacecraft spin-up. Cosmic Res., 34: 602-608.
    Direct Link  |  
  35. Levskii, M.V., 1995. Optimal control of the spatial turn of a spacecraft. Cosmic Res., 33: 452-456.