Zobrazeno 1 - 10
of 77
pro vyhledávání: '"V. N. Ryabchenko"'
Publikováno v:
Russian Aeronautics. 65:99-110
Publikováno v:
RUDENKO INTERNATIONAL CONFERENCE “METHODOLOGICAL PROBLEMS IN RELIABILITY STUDY OF LARGE ENERGY SYSTEMS” (RSES 2021).
Publikováno v:
RUDENKO INTERNATIONAL CONFERENCE “METHODOLOGICAL PROBLEMS IN RELIABILITY STUDY OF LARGE ENERGY SYSTEMS” (RSES 2021).
Publikováno v:
Russian Aeronautics. 64:432-440
Publikováno v:
Journal of Computer and Systems Sciences International. 59:845-853
An approach is proposed to identify abnormal modes of a power system in real time, using only the data of synchronized vector measurements and that does not require a priori information about the parameters of its mathematical model. The algorithmic
Publikováno v:
Russian Aeronautics. 63:249-259
The problem is analytically solved of synthesis of the longitudinal motion stabilization law of a single-rotor helicopter at the lack of information about the vertical speed of its motion. The solution is based on the method of output control synthes
Publikováno v:
Journal of Computer and Systems Sciences International. 59:151-160
A variant of the synthesis method for controlling a linear MIMO system by an output vector is developed that provides the given spectrum of a multidimensional dynamic system in the state space. It is based on the principle of duality of the task of c
Publikováno v:
Elektrichestvo. 6:6-12
The accident rate of overhead lines (OHL) of 500 kV of a large region over an extended time period was investigated. Significant fluctuations in the values of their failure flow parameter (failure frequency) were revealed. The indicated parameter was
Publikováno v:
Elektrichestvo. 9:4-10
The results from predicting the failure rate of 500 kV overhead power lines represented as a time series and having signs of its being chaotic in nature are presented. The predictive estimates were obtained using the regression (spectral singular ana
Publikováno v:
Journal of Computer and Systems Sciences International. 58:969-979
The problem of joint synthesis of a modal controller and observer is solved analytically for a sixth-order system that describes the rotational motion of a spacecraft with the available measurements of five components of the state vector. The modelin