Adaptation of Aircraft's Wings Elements in Turbulent Flows by Local Voting Protocol

Research output: Contribution to journalArticlepeer-review

3 Scopus citations

Abstract

Miniaturization and increased performance calculators, sensors and actuators are opening up the new possibilities of intelligent control complex mechatronic systems under the transient and turbulent conditions. Earlier adaptive control in a changing environment and with time-varying structure of the state space explored slightly due to the limited possibilities of practical implementation. The paper considers the model of an aircraft with a large number of sensors and actuators, distributed over surfaces of wings. In turbulent wind flows, it is shown that the multi-agent Local Voting Protocol with non-decreasing to zero step size allows equalization effects of disturbing forces acting on the different elements of wings.

Original languageEnglish
Pages (from-to)1904-1909
Number of pages6
JournalIFAC-PapersOnLine
Volume50
Issue number1
DOIs
StatePublished - 2017
Event20th World Congress of the International Federation of Automatic Control - Toulouse, France, Toulouse, France
Duration: 9 Jul 201714 Jul 2017
Conference number: 20

Scopus subject areas

  • Control and Systems Engineering

Keywords

  • Adaptation
  • Local Voting Protocol
  • non-equilibrium statistical mechanics
  • self-organization
  • turbulent wind flows

Fingerprint

Dive into the research topics of 'Adaptation of Aircraft's Wings Elements in Turbulent Flows by Local Voting Protocol'. Together they form a unique fingerprint.

Cite this