Optimization of the hierarchical system of "guidance-stabilization" of the aircraft with the stabilization system adaptation

The article describes the research technique to study the influence of the aircraft highly maneuverable trajectory on the dynamic inter-axis cross feeds of the three-channel stabilization system with the help of the methods of optimization of the multiobject multicriterion systems control under the conditions of structural inconsistencies. This method is used for optimization of the hierarchical control system ensuring coordinated steadily effective compromises based on hierarchical trims and the optimal control over the multiobject multicriterion level systems. The ways of establishing laws of the coordinated control and their parameterization are considered.

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