• DocumentCode
    3042305
  • Title

    A novel algorithm for optimal design of impulsive orbit transfer using multi-phase Gauss pseudospectral method

  • Author

    Shen, Hongxin

  • Author_Institution
    Nat. Univ. of Defense Technol., Changsha, China
  • fYear
    2010
  • fDate
    8-10 June 2010
  • Firstpage
    588
  • Lastpage
    592
  • Abstract
    A Gauss pseudospectral method (GPM) is presented for directly solving impulsive orbit transfer problem. The Gauss pseudospectral method is applied to the multi-phase optimal control problem; the model of multi-phase control linkage conditions and more flexible solving strategy are also presented. Two typical orbit transfer problems are studied, the simulation results are compared with the available numerical prediction, and show good accuracy, rapid convergence(time consumption is several seconds), robustness with initial guess, which means that the GPM can used to generate an optimal impulsive orbit transfer trajectory through the onboard computer.
  • Keywords
    aerospace control; control system synthesis; optimal control; position control; Gauss pseudospectral method; impulsive orbit transfer; multiphase optimal control problem; Accuracy; Couplings; Optimization; Orbits; Robustness; Space vehicles; Trajectory;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
  • Conference_Location
    Harbin
  • Print_ISBN
    978-1-4244-6043-4
  • Electronic_ISBN
    978-1-4244-7505-6
  • Type

    conf

  • DOI
    10.1109/ISSCAA.2010.5633101
  • Filename
    5633101