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A hybrid flight control for a simulated raptor-30 v2 helicopter.
Author(s):
1. Arbab Nighat Khizer: Department of Electrical Engineering, Mehran University of Engineering & Technology, Jamshoro, Pakistan
2. Amir Mahmood Soomro: Department of Electrical Engineering, Mehran University of Engineering & Technology, Jamshoro, Pakistan
3. Syed Amjad Ali: Department of Biomedical Engineering, Mehran University of Engineering & Technology Jamshoro, Pakistan
Abstract:
This paper presents a hybrid flight control system for a single rotor simulated Raptor-30 V2 helicopter. Hybrid intelligent control system, combination of the conventional and intelligent control methodologies, is applied to small model helicopter. The proposed hybrid control used PM as a traditional control and fuzzy as an intelligent control so as to take the maximum advantage of advanced control theory. The helicopter`s model used; comes from X-Plane flight simulator and their hybrid flight control system was simulated using MATLAB/SIMULINK in a simulation platform. X-Plane is also used to visualize the performance of this proposed autopilot design. Through a series of numerous experiments, the operation of hybrid control system was investigated. Results verified that the proposed hybrid control has an excellent performance at hovering flight mode. 
Page(s): 176-182
DOI: DOI not available
Published: Journal: Mehran University Research Journal of Engineering and Technology, Volume: 34, Issue: 2, Year: 2015
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