Main approaches and features of the design of aircraft hydro-mechanical control systems

Abstract

The main purpose of the article is to identify the main approaches and define the concept when modeling the hydro-mechanical control systems of an aircraft. The advantages and importance of a computational experiment with the aid of a virtual test bed at the stage of constructive parametric debugging of the elements of complex hydraulic systems are emphasized. The characteristics obtained from the results of the computational experiment will allow us to determine the level of adequacy of the models and subsequently choose the most optimal design and operational parameters.

Keywords

• electro-hydraulic servo drive
• experimental research
• numerical simulation
• computational experiment
• control system
• aircraft
• diagnostic modeling
• nonlinear phenomena
• hydraulic automation devices