Aiming at the optimization problem of spacecraft transfer trajectory, based on differential evolution algorithm, a fast optimization method for transfer trajectory with modified differential algorithm is proposed. The method can quickly find the best transfer trajectory that satisfies the specified constraints through the intelligent optimization based on the population individuals. It avoids the problems of large calculation and low efficiency caused by traditional iteration methods. The actual application of the calculation of the transfer trajectory under certain initial conditions shows that the method can quickly determine the transfer orbit parameters.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Calculation of Spacecraft Transfer Trajectory Based on Modified Differential Evolution Algorithm


    Weitere Titelangaben:

    Smart Innovation, Systems and Technologies


    Beteiligte:
    Wu, Tsu-Yang (Herausgeber:in) / Ni, Shaoquan (Herausgeber:in) / Chu, Shu-Chuan (Herausgeber:in) / Chen, Chi-Hua (Herausgeber:in) / Favorskaya, Margarita (Herausgeber:in) / Zheng, Gui-bo (Autor:in) / Yin, Qing (Autor:in) / Wu, Guan-qun (Autor:in) / Huang, Ke-yan (Autor:in)


    Erscheinungsdatum :

    2021-11-30


    Format / Umfang :

    9 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






    Spacecraft trajectory

    Horsewood, J. L. / Mann, F. J. | NTRS | 1980


    Spacecraft trajectory optimization

    Conway, Bruce A. | SLUB | 2010