Adaptive controller design based on time-scale-separation method for testbed of strength tests of aircraft structures

摘要

The paper is devoted to development of an universal firmware in order to carry out of strength and fatigue tests for aeronautical equipments. The framework of the developed firmware is described. The firmware is operated as the part of testbed and allows providing computer-aided strength and fatiguing tests. Hardware components of the firmware are based on industrial equipment which is used in stands for strength tests. The upper level of software is implemented by means of Visual Studio 2012 with C#, WPF, C++. The lower level of software is implemented by means of ANSI-C and PLC code. The created firmware allows increasing of implementation accuracy of power loading cyclograms during of strength and fatigue tests for aeronautical equipments.