• DocumentCode
    3350783
  • Title

    A Reentry Trajectory Planning Based on the Optimization of Angle of Attack

  • Author

    Zhuo, Yang ; Qingzhen, Zhang ; Xiaoqiang, Tao

  • Author_Institution
    Sch. of Autom. Sci. & Electr. Eng., BeiHang Univ., Beijing, China
  • fYear
    2011
  • fDate
    21-23 Oct. 2011
  • Firstpage
    937
  • Lastpage
    940
  • Abstract
    According to the strict aerodynamic heating environment in the reentry process, a new reentry trajectory planning method is presented. A reasonable Heat Flux Rate (HFR) curve is designed with the energy of the aircraft, and the real-time instruction of the Angle of Attack (AOA) is decoded. Then, the flight corridor is planned by the multi-constraint conditions. After that, the flight trajectory could be optimized through applying the pseudo-spectral method. At last, the simulation experiment under Matlab is carried out with an example lifting flight. The results show that the aircraft´s total heat absorption (THA), which got through the new planning method, is smaller than that by the traditional method.
  • Keywords
    absorption; aerodynamics; aircraft; planning; Matlab; aerodynamic heating environment; aircraft total heat absorption; angle of attack optimization; flight corridor; flight trajectory; heat flux rate curve; lifting flight; pseudo-spectral method; reentry trajectory planning method; Aircraft; Heating; Optimization; Planning; Real time systems; Trajectory; Vehicles; angle of attack (AOA); heat flux rate (HFR); lifting flight; reentry; trajectory planning;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation, Measurement, Computer, Communication and Control, 2011 First International Conference on
  • Conference_Location
    Beijing
  • Print_ISBN
    978-0-7695-4519-6
  • Type

    conf

  • DOI
    10.1109/IMCCC.2011.236
  • Filename
    6154262