Tracking control for planar nonminimum-phase bilinear control system with disturbance using backstepping

نویسندگان

چکیده

This article <span>presents the design control of a tracking problem for non-minimum phase bilinear system containing disturbance. The is assumed to have relative degree one and phase, which means it has unstable internal dynamics. disturbance exists only in state variables corresponding function external was carried out using backstepping method, applied normal form system. Internal dynamics will be stabilised virtual overcome last step stabilise original function. simulation results show that proposed method can rapidly drive output given trajectory. Control performance varies depending on parameter setting. higher parameter, better performance, evaluated integral absolute error.</span>

برای دانلود رایگان متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

NonLinear Predictive Control for a NonHolonomic Nonminimum Phase System

This work addresses the problem of nonlinear control of nonholonimic, nonminimum-phase systems . More speci cally, the problem of trajectory tracking for a motorcycle-like system will be considered. The literature on this topic appears to be rather limited, both with regard to the theorical side, as well as concerning the applications. The path is considered to be fully known in advance, in oth...

متن کامل

Voltage Control of Three Phase Inverters by Using Active Disturbance Rejection Control

Control of three phase inverters has been an important issue in recent years. This paper proposes active disturbance rejection control (ADRC) scheme for controlling three phase inverters. The main advantage of ADRC that motivated us for using this controller for inverter is that it is model independent.  This controller is used in a double loop structure including an inner current loop and oute...

متن کامل

Robust Backstepping Control of Wing Rock Using Disturbance Observer

Wing rock is a highly nonlinear phenomenon when the aircraft suffers undesired roll-dominated oscillatory at high angle of attack (AOA). Considering the strong nonlinear and unsteady aerodynamic characteristics, an uncertain multi-input and multi-output (MIMO) nonlinear wing rock model is studied, and system uncertainties, unsteady aerodynamic disturbances and external disturbances are consider...

متن کامل

Robust backstepping control for slew maneuver using nonlinear tracking function

The backstepping control method provides useful control logic, especially for a cascaded system. Because spacecraft dynamics and kinematics form a cascaded system, the spacecraft slew maneuver problem can be solved using the backstepping control method. However, the simple linear backstepping controller may result in poor design: sluggish motion, trivial nonlinear term cancellation, and excessi...

متن کامل

Relay Control with Parallel Compensator for Nonminimum Phase Plants

Following the Smith compensator the parallel compensator designed for difficult, e.g. nonminimum phase plants is applied to systems with relay control. The compensator connected in parallel to the plant changes its properties so that the replacement plant model becomes simpler and may be shaped dependently upon the goal of the control. In the case of regulation on a constant level a first order...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

ژورنال

عنوان ژورنال: Indonesian Journal of Electrical Engineering and Computer Science

سال: 2022

ISSN: ['2502-4752', '2502-4760']

DOI: https://doi.org/10.11591/ijeecs.v26.i3.pp1315-1327