• DocumentCode
    1410874
  • Title

    Autonomous formation flight

  • Author

    Giulietti, Fabrizio ; Pollini, Lorenzo ; Innocenti, Mario

  • Author_Institution
    Dept. of Electr. Syst. & Autom., Pisa Univ., Italy
  • Volume
    20
  • Issue
    6
  • fYear
    2000
  • fDate
    12/1/2000 12:00:00 AM
  • Firstpage
    34
  • Lastpage
    44
  • Abstract
    This article describes an approach to close-formation flight of autonomous aircraft. A standard LQ-based structure was synthesized for each vehicle and for formation position error control using linearized equations of motion and a lifting line model of the aircraft wake. We also consider the definition of a formation management structure, capable of dealing with a variety of generic transmission and communication failures among aircraft. The procedure was developed using a decentralized approach and relies on the Dijkstra algorithm. The algorithm provides optimal path information sequencing in the nominal case, as well as the redundancy needed to accommodate failures in data transmission and reception. Several simulations were carried out, and some of the results are presented. The overall scheme appears to be a valuable starting point for further research, especially specialization to situations representing more detailed and operational failures.
  • Keywords
    aircraft control; attitude control; decentralised control; linear quadratic control; optimisation; position control; Dijkstra algorithm; aircraft control; autonomous formation flight; decentralized control; lifting line model; linear quadratic control; optimisation; position control; Actuators; Aerospace control; Aircraft propulsion; Bandwidth; Control systems; Engines; Equations; Military aircraft; State feedback; Velocity control;
  • fLanguage
    English
  • Journal_Title
    Control Systems, IEEE
  • Publisher
    ieee
  • ISSN
    1066-033X
  • Type

    jour

  • DOI
    10.1109/37.887447
  • Filename
    887447