Hidden Nonlinear Oscillations in Controlled Aircraft with Saturated Inputs

Результат исследований: Публикации в книгах, отчётах, сборниках, трудах конференцийстатья в сборнике материалов конференции

1 цитирование (Scopus)

Выдержка

In the paper two types of nonlinear limit-cycles oscillations in flight control systems, caused by typical static nonlinearities of the control surfaces actuators that arise in the flight of aircraft are considered: The elastic-flexural flutter of the wing and pilot induced oscillations (PIO), where interactions of a flight controller with a human pilot's dynamics can cause the origin instability. Hidden oscillations in the pilot-aircraft closed loop are studied and localized by means of the iterative analytical-numerical method. A problem of adaptive flutter suppression is studied and an opportunity of emerging the hidden oscillations due to controlling surface saturation in rate and magnitude is demonstrated.

Язык оригиналаанглийский
Название основной публикации2018 15th International Conference on Control, Automation, Robotics and Vision, ICARCV 2018
ИздательInstitute of Electrical and Electronics Engineers Inc.
Страницы704-709
Число страниц6
ISBN (электронное издание)9781538695821
DOI
СостояниеОпубликовано - 18 дек 2018
Событие15th International Conference on Control, Automation, Robotics and Vision, ICARCV 2018 - Singapore, Сингапур
Продолжительность: 18 ноя 201821 ноя 2018

Конференция

Конференция15th International Conference on Control, Automation, Robotics and Vision, ICARCV 2018
СтранаСингапур
ГородSingapore
Период18/11/1821/11/18

Отпечаток

Nonlinear Oscillations
Aircraft
Oscillation
Flutter (aerodynamics)
Flutter
Flight control systems
Control nonlinearities
Control surfaces
Numerical methods
Actuators
Flight Control System
Controllers
Analytical Methods
Limit Cycle
Closed-loop
Saturation
Actuator
Numerical Methods
Nonlinearity
Controller

Предметные области Scopus

  • Искусственный интеллект
  • Компьютерное зрение и распознавание образов
  • Теория оптимизации

Цитировать

Andrievsky, B., Kuznetsov, N. V., & Kuznetsova, O. A. (2018). Hidden Nonlinear Oscillations in Controlled Aircraft with Saturated Inputs. В 2018 15th International Conference on Control, Automation, Robotics and Vision, ICARCV 2018 (стр. 704-709). [8581296] Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICARCV.2018.8581296
Andrievsky, Boris ; Kuznetsov, Nikolay V. ; Kuznetsova, Olga A. / Hidden Nonlinear Oscillations in Controlled Aircraft with Saturated Inputs. 2018 15th International Conference on Control, Automation, Robotics and Vision, ICARCV 2018. Institute of Electrical and Electronics Engineers Inc., 2018. стр. 704-709
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abstract = "In the paper two types of nonlinear limit-cycles oscillations in flight control systems, caused by typical static nonlinearities of the control surfaces actuators that arise in the flight of aircraft are considered: The elastic-flexural flutter of the wing and pilot induced oscillations (PIO), where interactions of a flight controller with a human pilot's dynamics can cause the origin instability. Hidden oscillations in the pilot-aircraft closed loop are studied and localized by means of the iterative analytical-numerical method. A problem of adaptive flutter suppression is studied and an opportunity of emerging the hidden oscillations due to controlling surface saturation in rate and magnitude is demonstrated.",
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Andrievsky, B, Kuznetsov, NV & Kuznetsova, OA 2018, Hidden Nonlinear Oscillations in Controlled Aircraft with Saturated Inputs. в 2018 15th International Conference on Control, Automation, Robotics and Vision, ICARCV 2018., 8581296, Institute of Electrical and Electronics Engineers Inc., стр. 704-709, Singapore, Сингапур, 18/11/18. https://doi.org/10.1109/ICARCV.2018.8581296

Hidden Nonlinear Oscillations in Controlled Aircraft with Saturated Inputs. / Andrievsky, Boris; Kuznetsov, Nikolay V.; Kuznetsova, Olga A.

2018 15th International Conference on Control, Automation, Robotics and Vision, ICARCV 2018. Institute of Electrical and Electronics Engineers Inc., 2018. стр. 704-709 8581296.

Результат исследований: Публикации в книгах, отчётах, сборниках, трудах конференцийстатья в сборнике материалов конференции

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N2 - In the paper two types of nonlinear limit-cycles oscillations in flight control systems, caused by typical static nonlinearities of the control surfaces actuators that arise in the flight of aircraft are considered: The elastic-flexural flutter of the wing and pilot induced oscillations (PIO), where interactions of a flight controller with a human pilot's dynamics can cause the origin instability. Hidden oscillations in the pilot-aircraft closed loop are studied and localized by means of the iterative analytical-numerical method. A problem of adaptive flutter suppression is studied and an opportunity of emerging the hidden oscillations due to controlling surface saturation in rate and magnitude is demonstrated.

AB - In the paper two types of nonlinear limit-cycles oscillations in flight control systems, caused by typical static nonlinearities of the control surfaces actuators that arise in the flight of aircraft are considered: The elastic-flexural flutter of the wing and pilot induced oscillations (PIO), where interactions of a flight controller with a human pilot's dynamics can cause the origin instability. Hidden oscillations in the pilot-aircraft closed loop are studied and localized by means of the iterative analytical-numerical method. A problem of adaptive flutter suppression is studied and an opportunity of emerging the hidden oscillations due to controlling surface saturation in rate and magnitude is demonstrated.

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Andrievsky B, Kuznetsov NV, Kuznetsova OA. Hidden Nonlinear Oscillations in Controlled Aircraft with Saturated Inputs. В 2018 15th International Conference on Control, Automation, Robotics and Vision, ICARCV 2018. Institute of Electrical and Electronics Engineers Inc. 2018. стр. 704-709. 8581296 https://doi.org/10.1109/ICARCV.2018.8581296