• DocumentCode
    1795251
  • Title

    Applications of homotopic approach in variable-specific-impulse low-thrust trajectory optimization

  • Author

    Li, J.F. ; Che, Z. ; Li, H.N.

  • Author_Institution
    State Key Lab. of Astronaut. Dynamics, Xi´an, China
  • fYear
    2014
  • fDate
    8-10 Aug. 2014
  • Firstpage
    2100
  • Lastpage
    2104
  • Abstract
    Homotopic approach can greatly reduce the difficulty of solving optimal control problems. Although the technology of solving fuel-optimal problem by starting from the related energy-optimal one is widely used in constant-specific-impulse low-thrust trajectory optimization, it is no longer applicable for variable-specific-impulse problems. For the variable-specific-impulse low-thrust trajectory optimization, the homotopic variable-specific-impulse thrust model is established by proposing a cubic function of thrust as homotopic function, and then the problem can be efficiently solved by homotopic alternate algorithm. The results demonstrate that this technique can improve the probability and efficiency of finding optimal solution.
  • Keywords
    aerospace propulsion; electric propulsion; optimal control; space vehicles; trajectory optimisation (aerospace); constant-specific-impulse low-thrust trajectory optimization; cubic function; energy-optimal problem; fuel-optimal problem; homotopic alternate algorithm; homotopic approach; optimal control problems; spacecraft electric propulsion system; variable-specific-impulse low-thrust trajectory optimization; Earth; Equations; Mathematical model; Optimal control; Optimization; Space vehicles; Trajectory;
  • 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.2014.7007501
  • Filename
    7007501