Affiliation:
1. LDEE Laboratory, University of Sciences and Technology of Oran Mohamed Boudiaf, Algeria
2. IBISC Laboratory, University of Evry Val d’Essonne, France
Abstract
In this article, we present the result of a nonlinear control technique applied to an autonomous quadrotor helicopter called X4-flyer. Using sliding mode-backstepping procedure, we can stabilize the engine in hovering mode. Moreover, for rejecting external load disturbance, two controls are presented: proportional-integral sliding mode-backstepping which is the combination between proportional-integral and sliding mode-backstepping into the so-called integral sliding mode-backstepping and the second is fuzzy integral sliding mode-backstepping. Finally fuzzy integral sliding mode-backstepping controller is investigated, where a fuzzy inference mechanism is used to achieve position tracking objective. The robustness of the controllers is studied in the presence of disturbances. Simulation results are also provided in order to illustrate the performances of the proposed controller versus the wind.
Subject
Mechanical Engineering,Aerospace Engineering
Cited by
19 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献