Sukhanov Viktor Min'onovich

Publications in Math-Net.Ru

1. Some Features of Powered Gyrostabilization of a Large Space Structure Assembled in Orbit
   
   Probl. Upr., 2016, no. 1,  82–89
2. Dynamic equations of free-flying space robot for feedback control tasks
   
   Avtomat. i Telemekh., 2015, no. 8,  153–164
3. Determination of workspace and required initial position of free-flying space manipulator at target capture
   
   Avtomat. i Telemekh., 2014, no. 11,  150–159
4. Some issues of controlling the free-flying manipulative space robot
   
   Avtomat. i Telemekh., 2013, no. 11,  62–83
5. Stabilization of low-frequency vibrations of a large satellite structure with powered gyro control
   
   Avtomat. i Telemekh., 2013, no. 3,  120–135
6. The comparative analysis of features of gyro-force control of large-scale spacecrafts for three algorithm types
   
   Probl. Upr., 2013, no. 4,  76–81
7. Combined relay-adaptive control of flexible spacecraft orientation
   
   Avtomat. i Telemekh., 2012, no. 12,  124–136
8. Dynamics of gyro-force stabilization of large-scale spacecrafts with use of adjusted PD-algorithm of control
   
   Probl. Upr., 2012, no. 5,  74–80
9. Using adaptation methods to stabilize elastic oscillations of large variable-parameter satellites
   
   Avtomat. i Telemekh., 2011, no. 12,  91–103
10. Physically realizable reference model-based algorithm of adaptive control
    
    Avtomat. i Telemekh., 2011, no. 8,  96–108
11. High-precision control of nonstationary aircrafts by roll angle
    
    Probl. Upr., 2011, no. 5,  82–87
12. Adaptive algorithm of attitude control for informational large-scale satellites with changing parameters
    
    Probl. Upr., 2011, no. 5,  74–81
13. Control of multimode manipulative space robot in outer space
    
    Avtomat. i Telemekh., 2010, no. 11,  96–111
14. Motion equations and control of the free-flying space manipulator in the reconfiguration mode
    
    Avtomat. i Telemekh., 2010, no. 1,  80–98
15. Design of discrete control system of flexible spacecraft maintaining robust stability of elastic oscillations
    
    Avtomat. i Telemekh., 2009, no. 7,  25–36
16. Design of modified PD algorithm to control angular motion of large space structure
    
    Avtomat. i Telemekh., 2009, no. 1,  39–50
17. Two-level orientation control system of flexible spacecraft with active stabilization of structural elastic oscillations
    
    Avtomat. i Telemekh., 2008, no. 6,  26–40
18. Dynamic features of flexible spacecraft control in process of its transformation into a large space structure
    
    Avtomat. i Telemekh., 2008, no. 5,  41–56
19. Formation of the control strategy for the large space structure assembled in orbit
    
    Avtomat. i Telemekh., 2007, no. 12,  21–37
20. Using the method of phase biplane to study dynamics of interactions of the elastic structural oscillations of the flexible spacecraft with the control system
    
    Avtomat. i Telemekh., 2007, no. 2,  49–62
21. Methods of intelligent diagnosis for control of flexible moving craft
    
    Avtomat. i Telemekh., 2006, no. 12,  3–20
22. Some questions of control of the robotized in-orbit assembly of large space structures
    
    Avtomat. i Telemekh., 2006, no. 8,  36–50
23. Computer-aided on-line development and derivation of the motion equation of space module
    
    Avtomat. i Telemekh., 2006, no. 1,  89–116
24. A method of generating the trajectory of in-orbit assembly of large space structures using the algorithms of optimization on graphs
    
    Avtomat. i Telemekh., 2005, no. 9,  12–26
25. Some features of the computer-aided derivation of the motion equations of a package of mechanical systems and their decomposition
    
    Avtomat. i Telemekh., 2005, no. 5,  83–96
26. Control of the angular motion of a semiactive bundle of bodies relying on the estimates of nonmeasurable coordinated obtained by Kalman filtration methods
    
    Avtomat. i Telemekh., 2005, no. 4,  156–169
27. Adaptive decomposing control algorithms for semiactive bundles of mechanical systems
    
    Probl. Upr., 2005, no. 3,  66–71
28. Fuzzy logic-based adaptive control system for in-orbit assembly of large space structures
    
    Avtomat. i Telemekh., 2004, no. 10,  109–127
29. A Method of Constructing the Mathematical Model of a Discretely Developing Large Space Structure
    
    Avtomat. i Telemekh., 2003, no. 10,  15–33
30. Application of the Principle of Design of Adaptive Systems with a Reference Model to Problems of Monitoring of a Current State of Transmission Shafts
    
    Avtomat. i Telemekh., 2003, no. 5,  131–146
31. New directions of adaptive coordinate-parametric control theory and applications
    
    Probl. Upr., 2003, no. 2,  2–10
32. Joint Estimation of the Motion Coordinates and Parameters of the Robotic Space Module and Transferred Elastic Load
    
    Avtomat. i Telemekh., 2002, no. 11,  88–102
33. On Technical Controllability and Decomposition of the Lagrangian Systems with Bounded Controls
    
    Avtomat. i Telemekh., 2002, no. 10,  13–33
34. Methods of Estimating the Envelope of Elastic Oscillations of the Flexible Spacecraft
    
    Avtomat. i Telemekh., 2002, no. 4,  76–90
35. Angular Motion Control of a Space Robot Engineering Module During Transportation of a Nonrigid Load
    
    Avtomat. i Telemekh., 2001, no. 11,  121–135
36. Technical Controllability of the Free-flying Automated Space Module
    
    Avtomat. i Telemekh., 2001, no. 3,  31–44
37. A dynamic model of a free-flying space robot engineering module
    
    Avtomat. i Telemekh., 2000, no. 5,  39–57
38. Adaptive and robust systems - Adaptive control of orientation of flexible spacecraft with variable parameters
    
    Avtomat. i Telemekh., 1999, no. 4,  90–102
39. Spatial angular motion of a flexible spacecraft: the modal-physical model and its characteristics
    
    Avtomat. i Telemekh., 1998, no. 12,  38–50
40. Design of an optimal mechanical structure of a free-flying space robotic module as a control object. II
    
    Avtomat. i Telemekh., 1998, no. 6,  75–88
41. Design of an optimal mechanical structure of a free-flying space robotic module as a control object. I
    
    Avtomat. i Telemekh., 1998, no. 5,  27–40
42. Large Space Constructions: Models, Research Methods, Control Principles. II
    
    Avtomat. i Telemekh., 1996, no. 8,  55–66
43. Large Space Constructions: Models, Research Methods, Control Principles. I
    
    Avtomat. i Telemekh., 1996, no. 7,  52–65
44. Parameter identification of a modal-physical model of a deformable spaceship
    
    Avtomat. i Telemekh., 1992, no. 7,  19–25