Krutova Inessa Nikolaevna

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. The comparative analysis of features of gyro-force control of large-scale spacecrafts for three algorithm types
   
   Probl. Upr., 2013, no. 4,  76–81
3. Dynamics of gyro-force stabilization of large-scale spacecrafts with use of adjusted PD-algorithm of control
   
   Probl. Upr., 2012, no. 5,  74–80
4. Adaptive algorithm of attitude control for informational large-scale satellites with changing parameters
   
   Probl. Upr., 2011, no. 5,  74–81
5. Design of discrete control system of flexible spacecraft maintaining robust stability of elastic oscillations
   
   Avtomat. i Telemekh., 2009, no. 7,  25–36
6. Design of modified PD algorithm to control angular motion of large space structure
   
   Avtomat. i Telemekh., 2009, no. 1,  39–50
7. Dynamic features of flexible spacecraft control in process of its transformation into a large space structure
   
   Avtomat. i Telemekh., 2008, no. 5,  41–56
8. Fuzzy logic-based design of the generalized adaptation algorithm for the discrete control system of flexible spacecraft
   
   Avtomat. i Telemekh., 2006, no. 6,  174–193
9. 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
10. Fuzzy logic-based adaptive control system for in-orbit assembly of large space structures
    
    Avtomat. i Telemekh., 2004, no. 10,  109–127
11. A Method of Constructing the Mathematical Model of a Discretely Developing Large Space Structure
    
    Avtomat. i Telemekh., 2003, no. 10,  15–33
12. A Fuzzy Logic Adaptation Circuit for Control Systems of Deformable Space Vehicles: Its Design
    
    Avtomat. i Telemekh., 2002, no. 7,  76–91
13. Stability Analysis of a Distorting Spacecraft Having Discrete Control System
    
    Avtomat. i Telemekh., 2001, no. 12,  40–54
14. On the stability of a spacecraft with regard for its elastic oscillations
    
    Avtomat. i Telemekh., 1999, no. 7,  44–58
15. Study of stabilization of the multidimensional dynamic system with relay control
    
    Avtomat. i Telemekh., 1999, no. 4,  27–43
16. Generation of an algorithm for the control of the iterative process of parameter adjustment in a system with a simplified reference model
    
    Avtomat. i Telemekh., 1998, no. 2,  72–84
17. The Use of a Simplified Reference Model in Tuning Control Parameters by the Adaptive Identification Method
    
    Avtomat. i Telemekh., 1997, no. 11,  131–144
18. Synthesis of a Control Algorithm for Iterative Tuning Parameters of a Dynamic System
    
    Avtomat. i Telemekh., 1997, no. 5,  12–27
19. Constructing the General Scheme of a Departmental Management System
    
    Avtomat. i Telemekh., 1996, no. 12,  124–144
20. Realization of Adjustable Properties of Aircraft Control Systems by the Method of Adaptive Identification
    
    Avtomat. i Telemekh., 1996, no. 3,  103–116
21. Parametric optimization of control algorithms by adaptive identification
    
    Avtomat. i Telemekh., 1995, no. 10,  107–120
22. Robustness of control systems with nonlinear parametric correction to some forms of disturbances
    
    Avtomat. i Telemekh., 1991, no. 9,  145–159
23. New aspects of dynamics of adaptive control systems with a reference model. II
    
    Avtomat. i Telemekh., 1986, no. 6,  107–119
24. New aspects of the dynamics of an adaptive control system with a standard model. I
    
    Avtomat. i Telemekh., 1986, no. 5,  70–81
25. Investigation of identification processes with the use of a parametric linearized model
    
    Avtomat. i Telemekh., 1982, no. 11,  81–90
26. The structure of a plant parameter identifier for an adaptive system from the class of nonsearching self adjusting systems
    
    Avtomat. i Telemekh., 1982, no. 5,  127–137
27. Structural investigation of self-adjusting systems
    
    Avtomat. i Telemekh., 1978, no. 12,  89–97
28. A linear model of an NSAS with the frequency response monitored
    
    Avtomat. i Telemekh., 1976, no. 7,  68–75
29. Design of linear models of nonsearching self-adjusting systems. II. Linear models of NSAS
    
    Avtomat. i Telemekh., 1976, no. 2,  116–130
30. Design of linear models for nonsearching self-adjucting systems. I. Linearized equations of NSAS
    
    Avtomat. i Telemekh., 1976, no. 1,  106–116