Designing and Modeling a Control System for Aircraft in the Presence of Wind Disturbance
محل انتشار: ماهنامه بین المللی مهندسی، دوره: 30، شماره: 12
سال انتشار: 1396
نوع سند: مقاله ژورنالی
زبان: انگلیسی
مشاهده: 384
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شناسه ملی سند علمی:
JR_IJE-30-12_006
تاریخ نمایه سازی: 1 اردیبهشت 1397
چکیده مقاله:
This paper proposes a switching adaptive control for trajectory tracking of unmanned aircraft systems. The switching adaptive control method is designed to overcome the wind disturbance and achieve a proper tracking performance for control systems. In the suggested system, the wind disturbance is regarded as a finite set of uncertainties; a controller is designed for each uncertainty, and a performance signal is obtained for switching between controllers through a set of visualizers. Each sub-system is robustly stable and the hysteresis logic-based switching is used to obtain the stabilization of a general system. The new system indicates more appropriate results for overcoming the air disturbance compared with the back-stepping adaptive controllers. Finally, the modeling results for the performance of the designed controller are presented
کلیدواژه ها:
نویسندگان
H Hamidi
Department of Industrial Engineering, Information Technology Group, K. N. Toosi University of Technology, Tehran, Iran
H Mortazave
Department of Electrical Engineering, South Tehran Branch, Islamic Azad University, Tehran, Iran
A Salahshoor
Department of Industrial Engineering, Information Technology Group, K. N. Toosi University of Technology, Tehran, Iran