Designing multi-flight control systems under uncertainty with the help of nu-synthesis
DOI:
https://doi.org/10.18372/2306-1472.36.1595Abstract
The purpose of this paper – is to expound the method of synthesis of algorithm of control and stabilization of motion of the multidimensional, quasi-optimal (nearly optimal) system. The presence of uncertainty with the simulated dynamics and action of perturbation factors are also foreseen in the object. The dynamics of the system is explored and it is shown that algorithms based on μ-approach, results in the system possessing property of weak sensitiveness to stochastic perturbations and provide high stability of dynamic behavior. This method is examined in application to the task of stabilizing of motion of «Navіon» monoplane. The results of mathematical simulation of control processes are shown.
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