Performance improvement of aircraft pitch angle using the fractional order adaptive PID controller

• Autorzy: Bensafia Yassine , Idir Abdelhakim , Zemmit Abderrahim , Khettab Khatir

Identyfikatory

DOI

10.15199/48.2023.05.18

Warianty tytułu

PL

Poprawa wydajności kąta nachylenia samolotu za pomocą adaptacyjnego kontrolera PID rzędu ułamkowego

• Języki publikacji: EN

Abstrakty

EN

Fractional calculus has been rediscovered by scientists and engineers in the last two decades, and applied in an increasing number of fields, namely control theory. The current research work presents the use of the fractional adaptive PID controller approach optimized by a genetic algorithm to improve the performances (rise time, setting time, overshoot, and mean absolute error) for aircraft by introducing a fractional order integrator and differentiator in the classical feedback adaptive PID controller. To validate the arguments, the effectiveness and performance analysis of the proposed fractional order adaptive PID controller optimized by a genetic algorithm have been studied in comparison to the classical adaptive PID controller. Numerical simulation and analysis are presented to verify the best controller. The fractional order adaptive PID gives the best results in terms of settling time, rise time, overshoot, and mean absolute error. This approach can also be generalized to other fractional and integer systems in order to improve their performances and noise rejection.

PL

Rachunek ułamkowy został na nowo odkryty przez naukowców i inżynierów w ciągu ostatnich dwóch dekad i stosowany w coraz większej liczbie dziedzin, a mianowicie w teorii sterowania. Obecna praca badawcza przedstawia zastosowanie podejścia adaptacyjnego regulatora PID ułamkowego zoptymalizowanego przez algorytm genetyczny w celu poprawy wydajności (czas narastania, czas ustawiania, przeregulowanie i średni błąd bezwzględny) dla samolotów poprzez wprowadzenie integratora i różniczkowania ułamkowego rzędu w klasycznym adaptacyjnym regulatorze PID ze sprzężeniem zwrotnym . Aby potwierdzić te argumenty, przeprowadzono analizę skuteczności i wydajności proponowanego adaptacyjnego regulatora PID ułamkowego rzędu zoptymalizowanego algorytmem genetycznym w porównaniu z klasycznym adaptacyjnym regulatorem PID. Przedstawiono symulację i analizę numeryczną w celu weryfikacji najlepszego sterownika. Adaptacyjny PID ułamkowego rzędu daje najlepsze wyniki pod względem czasu ustalania, czasu narastania, przeregulowania i średniego błędu bezwzględnego. To podejście można również uogólnić na inne systemy ułamkowe i całkowite w celu poprawy ich wydajności i tłumienia szumów.

Słowa kluczowe

EN

fractional system; aircraft system; fractional adaptive PID controlle; optimization

PL

system ułamkowy; system lotniczy; kontrolery frakcyjno-adaptacyjne PID; optymalizacja

• Wydawca: Wydawnictwo SIGMA-NOT
• Czasopismo: Przegląd Elektrotechniczny
• Rocznik: 2023
• Tom: R. 99, nr 5
• Strony: 98--101
• Opis fizyczny: Bibliogr. 29 poz., rys., tab.

Twórcy

autor

Bensafia Yassine

• Electrical Engineering Department, University of Bouira - Algeria

• https://orcid.org/0000-0003-1760-3636

autor

Idir Abdelhakim

• Electrical Engineering Department, Mohamed Boudiaf University of M’sila - Algeria
• Applied Automation Laboratory, F.H.C., University of Boumerdes, 35000 Boumerdes, Algeria

• https://orcid.org/0000-0002-3510-5932

autor

Zemmit Abderrahim

• Electrical Engineering Department, Mohamed Boudiaf University of M’sila - Algeria

• https://orcid.org/0000-0002-2365-0378

autor

Khettab Khatir

• Electrical Engineering Department, Mohamed Boudiaf University of M’sila - Algeria
• GE laboratory, University of M’sila, 28000 – Algeria

• https://orcid.org/0000-0003-2985-0466

Bibliografia

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