DOI

In the paper, the control problem with limitations on the magnitude and rate of the control action in aircraft control systems, is studied. Existence of hidden limit cycle oscillations in the case of actuator position and rate limitations is demonstrated by the examples of piloted aircraft PIO phenomenon and the airfoil flutter suppression system.

Original languageEnglish
Title of host publicationICNPAA 2018 World Congress
Subtitle of host publication12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences
EditorsSeenith Sivasundaram
PublisherAmerican Institute of Physics
Volume2046
ISBN (Electronic)9780735417724
DOIs
StatePublished - 4 Dec 2018
Event12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2018 - Yerevan, Armenia
Duration: 3 Jul 20186 Jul 2018

Conference

Conference12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences, ICNPAA 2018
Country/TerritoryArmenia
CityYerevan
Period3/07/186/07/18

    Scopus subject areas

  • Physics and Astronomy(all)

ID: 38483890