• DocumentCode
    2919161
  • Title

    An Analytic Solution of Entry Trajectory Based on Dynamic Pressure Planning

  • Author

    Wu, Liaoni ; Huang, Yimin ; He, Chenglong

  • Author_Institution
    Coll. of Autom. Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing
  • fYear
    2009
  • fDate
    20-22 Feb. 2009
  • Firstpage
    69
  • Lastpage
    72
  • Abstract
    An analytic trajectory solution based on dynamic pressure planning is presented for the gliding entry of lift-body. Firstly, the equations of motion are transformed from velocity to dynamic pressure and from time to altitude. An analytic method is proposed to calculate the trim angle-of-attack and other trajectory parameters based on dynamic pressure profile. Secondly, according the flight characteristics the entry is divided by initial descent and equilibrium glide. The dynamic pressure of equilibrium glide is scheduled and the geometric trajectory is calculated. Lastly, the simulation result shows that the trajectory design method is well satisfied the requirement of gliding entry.
  • Keywords
    position control; space vehicles; vehicle dynamics; analytic method; dynamic pressure planning; entry trajectory; equilibrium glide; geometric trajectory; trajectory design method; Aerodynamics; Design methodology; Differential equations; Dynamic scheduling; Earth; Technology planning; Trajectory; Transforms; Vehicle dynamics; Vehicles; Reentry; dynamic pressure planning; lift-body vehicle; trajectory design;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electronic Computer Technology, 2009 International Conference on
  • Conference_Location
    Macau
  • Print_ISBN
    978-0-7695-3559-3
  • Type

    conf

  • DOI
    10.1109/ICECT.2009.36
  • Filename
    4795922