A blended sliding mode control with linear quadratic integral control based on reduced order model for a VTOL system

Abstract:

In this paper, a Sliding Mode Control with chattering reduction based on reduced order model using Linear Quadratic Integral Control as sliding surface, is implemented to One Degree of Freedom Vertical Take-Off Landing System (VTOL). The controller performance is measured using Integral of the Square Error index by simulation and real tests. Finally, the Sliding Mode Control with a Linear Quadratic Integral Control as sliding surface performance for reference tracking and, robustness against VTOL system physical parameter uncertainties and external disturbances are verified by experimental results.

Año de publicación:

2017

Keywords:

• Reduced order model
• LQI
• ISE index
• sliding mode control
• VTOL System

Fuente:

scopus