Finite Time Terminal Synergetic Controller for Nonlinear Helicopter Model

被引：4

作者：

Ahifar, A. ^{[1
]}

Ranjbar, A. N. ^{[1
]}

Rahmani, Z. ^{[1
]}

机构：

[1] Babol Noshirvani Univ Technol, Control Grp, Fac Elect Engn, Babol Sar, Iran

来源：

INTERNATIONAL JOURNAL OF ENGINEERING | 2019年 / 32卷 / 02期

关键词：

Helicopter; Nonlinear Model; Multi Input-Multi Output; Synergetic Control; DESIGN;

D O I：

10.5829/ije.2019.32.02b.08

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

In this paper, an almost new control approach called terminal synergetic control which works based on user defined manifold is applied to a nonlinear helicopter model. Stability analysis is convestigated using Lyapunov stability theory. Synergetic controller is applied to this nonlinear fifth-order helicopter model to control height and angle. Simulation results showed that it has faster and smoother response in tracking reference inputs in comparison to sliding mode control, intelligent autopilot controller and feedback linearization method.

引用

页码：236 / 241

页数：6

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