Antonov V. Systems of stabilization and identification of flying vehicles with specified quality of transients

Українська версія

Thesis for the degree of Doctor of Science (DSc)

State registration number

0513U000473

Applicant for

Specialization

  • 05.07.01 - Аеродинаміка та газодинаміка літальних апаратів

25-04-2013

Specialized Academic Board

Д 26.062.05

Essay

The methods of synthesis of optimal control of an aircraft at the given motion quality and limited rudders deviations and adaptive identification with the optimal choice of control are proposed. The nonstationary components of aerodynamic characteristics of aircraft are calculated. A new problem of structural identification - definition of orders of derivatives for a customized model - is solved. Layouts of the aircrafts for heavy missiles air launch are proposed, the effectiveness of the developed methods for the synthesis of controllers for these objects in stabilizing a given height is shown.

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