• DocumentCode
    1795193
  • Title

    Modeling method for gliding reentry vehicle via model migration

  • Author

    Haoliang Wang ; Qingdong Li ; Zhang Ren ; Zixuan Liang

  • Author_Institution
    Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China
  • fYear
    2014
  • fDate
    8-10 Aug. 2014
  • Firstpage
    1739
  • Lastpage
    1743
  • Abstract
    The development of gliding reentry vehicle is a process of small-batch and multi-batch. In order to reduce the cost of experiments and shorten the cycle of modeling of gliding reentry vehicles with similar shapes, the new method based on model migration is presented in this paper. Specifically, a method of assessing the similarity degree of the gliding reentry vehicles is explained; whether the model migration theory can be applied in the vehicle modeling depends on the degree. The aerodynamic coefficients of the base gliding reentry vehicle are partitioned by the linearity of itself, and the cluster centers of the intervals are obtained. The migration equations are given through the analysis of the relation of the cluster centers of aerodynamic coefficients of the base vehicle to the ones of the new vehicle. The advantage of the new method is verified by the simulation.
  • Keywords
    entry, descent and landing (spacecraft); vehicle dynamics; aerodynamic coefficients; base gliding reentry vehicle modeling method; cost reduction; interval cluster centers; model migration theory; multibatch process; small-batch process; Aerodynamics; Atmospheric modeling; Linearity; Mathematical model; Numerical models; Shape; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
  • Conference_Location
    Yantai
  • Print_ISBN
    978-1-4799-4700-3
  • Type

    conf

  • DOI
    10.1109/CGNCC.2014.7007445
  • Filename
    7007445