AUTOPILOT DESIGN USING SMOOTH FRACTIONAL ORDER SLIDING MODE CONTROL

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AHMADI PEYMAN; VALI AHMADREZA; BEHNAMGOL VAHID

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Journal Paper

Paper Information

Journal: JOURNAL OF NONLINEAR SYSTEMS IN ELECTRICAL ENGINEERING Year:2018 | Volume:4 | Issue:1-2 Page(s): 63-77

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Title

AUTOPILOT DESIGN USING SMOOTH FRACTIONAL ORDER SLIDING MODE CONTROL

Author(s)

AHMADI PEYMAN | VALI AHMADREZA | BEHNAMGOL VAHID | Issue Writer Certificate

Keywords

FRACTIONAL ORDER CONTROL

SLIDING MODE CONTROL

CHATTERING PHENOMENA

AUTOPILOT

Abstract

In this paper, the fractional order SLIDING MODE CONTROL is used to design an aircraft AUTOPILOT. This method aims at reducing the chattering phenomenon and has smoother control signal than conventional sliding mode. FRACTIONAL ORDER CONTROL uses fractional integrator and derivative to improve integer order control methods. The sliding surface and SLIDING MODE CONTROL law are proposed to reduce the chattering phenomenon, while the closed-loop stability is guaranteed. Using this algorithm, a robust AUTOPILOT against aerodynamic coefficients uncertainties is designed for an aircraft and the proposed control law is utilized to stabilize the closed loop system by the Lyapunov stability theorem. The proposed AUTOPILOT is applied to the aircraft model and our simulation results illustrate the reduction of chattering phenomenon.

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