Optimum Average of High-Speed to Describe of Aircraft by the Flying-Tests

Abstract

In determinate models of control dynamic objects usage minimum of information operating physical factors. Criterions orthogonal tests of optimization should be damage enter probable (density of probability), or another realization of vector accidental indignation and application put into practice, example object of control type aircraft. Example variable (unsteady) control of factor aircraft (realization accidental of parameters) should be guarantee execution concrete of realization purposes, even in maximum be in difficulties. This demand include in number criterions of optimization achievement extreme of expectation value of quality functional of object of control. Application flight fitness probability achievement execution completion of mission. Definition irregularity control of decision with take into consideration should be name problem optimum mean quantity or statistical optimization of dynamic system. By the solution statistical problem optimization arise news enough session difficulties. She connected with decision theoretical questions, which now should be by the analysis of determinate models and organization of quality procedure. Latter procedure realization by the considerable increase machine time and including methods statistical simulation (artificial reproduction) of property object of control (aircraft). Application criterion statistical optimization propose, what beforehand (in good time) statistical according to official returns. Receipt of statistical information realization analysis of experience developmental. Methods optimization propose arbitrary law of random characteristic. Reliable of conclusions under certain conditions possess statistical characteristic.