• DocumentCode
    690368
  • Title

    Research on Climb Performance and 4D Trajectory Prediction of Aircraft

  • Author

    Xiaoyan Zhang ; Yunxiang Han

  • Author_Institution
    Coll. of Air Traffic Manage., Civil Aviation Flight Univ. of China, Deyang, China
  • fYear
    2013
  • fDate
    14-15 Dec. 2013
  • Firstpage
    390
  • Lastpage
    393
  • Abstract
    4D reckoning is a core technology to the next generation of air transport management. This paper mainly do research on the aircraft dynamics model under a given flight profile of different phases of flight performance and aircraft performance differences. Then, proposed two models: state switching transition model between different phases of flight, System evolution model under the continuous variation states that aircraft weight, indicated airspeed, altitude, distance and others. Using the mode of hybrid system recursive simulation obtained 4D trajectory of aircraft and analyzed the effects of various factors on the performance of the aircraft´s climb.
  • Keywords
    aircraft; recursive estimation; vehicle dynamics; air transport management; aircraft 4D trajectory prediction; aircraft altitude; aircraft climb performance; aircraft distance; aircraft dynamics model; aircraft indicated airspeed; aircraft weight; continuous variation states; flight performance; flight profile; hybrid system recursive simulation; state switching transition model; system evolution model; Air traffic control; Aircraft; Atmospheric modeling; Educational institutions; Fuels; Mathematical model; Trajectory; 4D trajectory; a new generation of air traffic control automation system; climb performance; hybrid system model;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Computer Sciences and Applications (CSA), 2013 International Conference on
  • Conference_Location
    Wuhan
  • Type

    conf

  • DOI
    10.1109/CSA.2013.98
  • Filename
    6835625