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computation
II International Conference "Parallel Computation and Control Problems" PACO'2004
      
A method of price computation with regard for the fuel consumption of generating units and load types is described.
      
Computation scheduling in multiprocessor real-time automatic control systems with constrained processor memory
      
Computation of dynamic characteristics of control systems: An Effectiveness enhancement method
      
This method enhances the accuracy of computation of dynamic characteristics at least by 20%.
      
An algorithm, which is stable to information noises and computation errors, is designed for solving the problem of control under incomplete information on the phase trajectory (measurements of part of coordinates).
      
Recurrence formulas for computation of the empty system probability and some other performance characteristics of the system, are determined.
      
Current problems in parallelization of the computation algorithms and organization of parallel computations
      
Practical criteria for stability of the linear dynamic system were proposed on the basis of the iterative procedure for computation of the matrix sign function.
      
Computation of phase and noise characteristics of the playback by taking fluctuations of the sawtooth transition in digital magn
      
A computation of phase, amplitude, and noise characteristics of the quantity of the sawtooth transition parameters is performed.
      
Direct computation demonstrated that the correlation coefficient can also be considered as an index of competition, and its dynamics is indeed non-monotone in uniform communities.
      
Computation of entropy contribution to protein-ligand binding free energy
      
Rapidly Convergent Series for the Computation of the Interaction Energy between Dissimilar Plane Parallel Double Layers
      
A comparison of the estimate with the results of numerical computation is carried out.
      
Comparison of the results of the computation on a digital computer with the experimental data show the effectiveness of this method for determining the structure of the initial section of such an axisymmetric jet.
      
A difference scheme which permits computation without change in grid parameters over the entire range from equilibrium to frozen flow regimes is used to solve the equations of the chemically non-equilibrium boundary layer.
      
At the same time it is obvious that the solution of these problems for irregular media and particularly the determination of their effective characteristics requires the use of statistical methods of computation.
      
The methods, based on the lifting surface scheme and the use of discrete vortical singularities, enable quite efficient and reliable digital computation of the flow about these wings at moderate angles of attack.
      
The velocity field is determined by numerical differentiation, which reduces the computation accuracy significantly.
      
 

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