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The paper describes the influence of power line elements on the power supply output for mechatronic modules. The weight-size parameters for advanced actuators of control systems of aircraft mechatronic modules can be determined by the amount of power consumed by each element of the actuator.
Based on an integrated approach, we solve the optimization problem for energy content and weight-dimensional characteristics of the electric servo drive by synthesis of structure and analysis of characteristics for different power supplies. The generalized power supply model, developed for different power supply of drive control systems, is given.
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