Adaptive PID Control for an Airplane plus Pilot Using RLS and LS algorithm
Publish Year: 1400
نوع سند: مقاله کنفرانسی
زبان: English
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شناسه ملی سند علمی:
AEROSPACE19_206
تاریخ نمایه سازی: 10 دی 1400
Abstract:
PID controllers are simple and straightforward to use; that’s why they play a vital role in industrial applications. In this paper, an adaptive PID controller is used to control aircraft roll and yaw modes in the presence of a pilot. The pilot transfer function makes the controller design more realistic. Both RLS and LS methods are used to estimate and adjust PID controller parameters in real-time, based on reference model output. An aircraft is simulated and controlled by this method, and the results indicate APID superiority in comparison to traditional PID
Keywords:
Adaptive PID-Pilot Model-RLS-LS-Roll and yaw response
Authors
Vahid Kh.Marefat
Mechanical Engineering Department, Urmia University of Technology
Hamed Ghaffari
Faculty of new science and technologies, University of Tehran