• DocumentCode
    233389
  • Title

    Air conflict resolution algorithm based on optimal control

  • Author

    Lu Yanjun ; Zhang Bo ; Zhang Xiaodong

  • Author_Institution
    Sch. of Autom., Shenyang Aerosp. Univ., Shenyang, China
  • fYear
    2014
  • fDate
    28-30 July 2014
  • Firstpage
    8919
  • Lastpage
    8923
  • Abstract
    In order to address the issue of conflict resolution between aircrafts, an improved algorithm based on optimal control theory is presented by which collision avoidance with other aircraft could be achieved with a minimum change on the original route. At first, an optimal escape maneuver is formulated to be a variable terminal-time optimal control problem with a compound performance index. Secondly the model of conflict resolution is set up, which is combined with the dynamics model of an aircraft. Finally, according to minimum principle, the optimal control problem is solved and consequently an optimal route is obtained. Simulation results show that for a collision danger in air with different flight heading or altitude, the algorithm could give an optimal route for conflict resolution.
  • Keywords
    aircraft control; collision avoidance; minimum principle; time optimal control; vehicle dynamics; air conflict resolution algorithm; aircraft dynamics model; collision avoidance; compound performance index; minimum principle; optimal escape maneuver; variable terminal-time optimal control problem; Aerospace control; Aircraft; Atmospheric modeling; Collision avoidance; Equations; Mathematical model; Optimal control; Conflict Resolution; Optimal Control; Optimal Route;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2014 33rd Chinese
  • Conference_Location
    Nanjing
  • Type

    conf

  • DOI
    10.1109/ChiCC.2014.6896501
  • Filename
    6896501