The application of genetic algorithm is discussed in the problem of minimum-fuel consumption orbit manoeuvre of spacecraft. First, the method of operation is introduced. Two examples are then given: one is soft-landing of a lunar probe from lunar satellite orbit to lunar surface; and the other is orbit manoeuvre of lunar probe from a selenocentric hyperbolic orbit to a selenocentric circular orbit. It is shown that the genetic algorithm has good convergence property and high accuracy.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Use of genetic algorithm in optimal orbit manoeuvre


    Contributors:
    Guoqiang Zeng, (author) / Xiaoning Xi, (author) / Xuan Ren, (author)


    Publication date :

    2000-01-01


    Size :

    356839 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    The Optimal Manoeuvre

    Biral, Francesco / Bertolazzi, Enrico / Mauro, Da Lio | Wiley | 2014


    Orbit Control Manoeuvre Strategy for EarthCARE

    Ormston, Thomas / Kuijper, Dirk / Mardle, Nic | AIAA | 2014


    Entering lunar orbit: the LOI manoeuvre

    Woods, W. David | Springer Verlag | 2008


    Strategies for Orbit Injection that Includes Yaw Manoeuvre

    De Castro Leite Filho, W. | British Library Online Contents | 1997