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:: Volume 4, Issue 1 (3-2018) ::
JNSEE 2018, 4(1): 63-77 Back to browse issues page
Autopilot Design Using Smooth Fractional Order Sliding Mode Control
Peyman Ahmadi, Ahmad-Reza Vali , Vahid Behnamgol
Malek Ashtar University of Technology , ar.vali@aut.ac.ir
Abstract:   (5043 Views)

In this paper, a new combination of fractional order calculus and finite time sliding mode control, used to design an aircraft autopilot. This combination aims to reduce the chattering phenomena and have a smoother control signal than conventional sliding mode. Fractional order control uses fractional integrator and derivative to improved integer order control methods. The sliding surface and sliding mode control law is proposed to reduce the chattering phenomena and also, closed-loop stability is guaranteed too. Using this algorithm, a robust autopilot against aerodynamic coefficients uncertainty is designed for an aircraft and proposed control law is utilized to stabilize the close loop system by Lyapunov stability theorem. The proposed autopilot is applied to the aircraft model and simulation results illustrate the reduction of chattering phenomena.

Keywords: Fractional order control, Sliding mode control, chattering phenomena, Missile autopilot
Full-Text [PDF 977 kb]   (1273 Downloads)    
Type of Study: Research | Subject: Nonlinear Control
Received: 2015/07/23 | Accepted: 2016/02/3 | Published: 2018/05/7
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ahmadi P, Vali A, Behnamgol V. Autopilot Design Using Smooth Fractional Order Sliding Mode Control. JNSEE. 2018; 4 (1) :63-77
URL: http://jnsee.sut.ac.ir/jnsee/article-1-130-en.html

Volume 4, Issue 1 (3-2018) Back to browse issues page
سامانه های غیرخطی در مهندسی برق Journal of Nonlinear Systems in Electrical Engineering
نشریه سامانه‌های غیرخطی در مهندسی برق در خصوص اصول اخلاقی انتشار مقاله، از توصیه‌های «کمیته بین‌المللی اخلاق نشر» موسوم به COPE و «منشور و موازین اخلاق پژوهش» مصوب معاونت پژوهش و فناوری وزارت علوم، تحقیقات و فناوری تبعیت می‌کند.
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