Pilot-Induced Oscillation Suppression by Using 𝐿1 Adaptive Control

Despite significant technical advances, pilot-induced oscillation (PIO) continues to occur in both flight tests and operational aircrafts. Such a phenomenon has led to significant research activities that aim to alleviate this problem. In this paper, the L1 adaptive controller has been introduced to...

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Main Authors: Chuan Wang, Michael Santone, Chengyu Cao
Format: Article
Language:English
Published: Wiley 2012-01-01
Series:Journal of Control Science and Engineering
Online Access:http://dx.doi.org/10.1155/2012/394791
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author Chuan Wang
Michael Santone
Chengyu Cao
author_facet Chuan Wang
Michael Santone
Chengyu Cao
author_sort Chuan Wang
collection DOAJ
description Despite significant technical advances, pilot-induced oscillation (PIO) continues to occur in both flight tests and operational aircrafts. Such a phenomenon has led to significant research activities that aim to alleviate this problem. In this paper, the L1 adaptive controller has been introduced to suppress the PIO, which is caused by rate limiting and pure time delay. Due to its architecture, the L1 adaptive controller will achieve a desired response with fast adaptation. The analysis of PIO and its suppression by L1 adaptive controller are presented in detail in the paper. The simulation results indicate that the L1 adaptive control is efficient in solving this kind of problem.
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spelling doaj-art-ea2d1bfad2ff44b4b5d3fc74c75aaf1e2025-08-20T02:21:46ZengWileyJournal of Control Science and Engineering1687-52491687-52572012-01-01201210.1155/2012/394791394791Pilot-Induced Oscillation Suppression by Using 𝐿1 Adaptive ControlChuan Wang0Michael Santone1Chengyu Cao2Department of Mechanical Engineering, University of Connecticut, Storrs, CT 06269-3139, USADepartment of Mechanical Engineering, University of Connecticut, Storrs, CT 06269-3139, USADepartment of Mechanical Engineering, University of Connecticut, Storrs, CT 06269-3139, USADespite significant technical advances, pilot-induced oscillation (PIO) continues to occur in both flight tests and operational aircrafts. Such a phenomenon has led to significant research activities that aim to alleviate this problem. In this paper, the L1 adaptive controller has been introduced to suppress the PIO, which is caused by rate limiting and pure time delay. Due to its architecture, the L1 adaptive controller will achieve a desired response with fast adaptation. The analysis of PIO and its suppression by L1 adaptive controller are presented in detail in the paper. The simulation results indicate that the L1 adaptive control is efficient in solving this kind of problem.http://dx.doi.org/10.1155/2012/394791
spellingShingle Chuan Wang
Michael Santone
Chengyu Cao
Pilot-Induced Oscillation Suppression by Using 𝐿1 Adaptive Control
Journal of Control Science and Engineering
title Pilot-Induced Oscillation Suppression by Using 𝐿1 Adaptive Control
title_full Pilot-Induced Oscillation Suppression by Using 𝐿1 Adaptive Control
title_fullStr Pilot-Induced Oscillation Suppression by Using 𝐿1 Adaptive Control
title_full_unstemmed Pilot-Induced Oscillation Suppression by Using 𝐿1 Adaptive Control
title_short Pilot-Induced Oscillation Suppression by Using 𝐿1 Adaptive Control
title_sort pilot induced oscillation suppression by using 𝐿1 adaptive control
url http://dx.doi.org/10.1155/2012/394791
work_keys_str_mv AT chuanwang pilotinducedoscillationsuppressionbyusingl1adaptivecontrol
AT michaelsantone pilotinducedoscillationsuppressionbyusingl1adaptivecontrol
AT chengyucao pilotinducedoscillationsuppressionbyusingl1adaptivecontrol