DESIGN FAST TERMINAL SLIDING MODE CONTROLLER OF WINDING SYSTEMS FOR ELASTIC WEBS

Authors

  • Trần Xuân Tình
  • Phạm Tuấn Thành

Keywords:

Backstepping controller, Receding Horizon Optimal, aircraft, altitude, flight path angle.

Abstract

The paper presents the results of fast terminal sliding mode controller based
on linear matrix inequality with high gain observer winding systems for elastic
webs. The results surveyed and evaluated by simulation on Matlab-Simulink
software show that the controller ensures the quality requirements in the system
under the influence of nonlinear factors as causing the mechanical structure.

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Published

2023-04-04

Issue

Section

RESEARCH AND DEVELOPMENT