The powered descent phase is the terminal phase of the planetary descent and landing mission, where the required direction and magnitude of the thrust engine are determined to steer the spacecraft to meet the pre-determined targeting condition at the end, such as touchdown at the designated landing site with the required velocity [12].


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    Titel :

    Simultaneous Trajectory Optimization for Adaptive Powered Descent


    Weitere Titelangaben:

    Springer ser. in Astrophysics & Cosmology


    Beteiligte:
    Song, Zhengyu (Herausgeber:in) / Zhao, Dangjun (Herausgeber:in) / Theil, Stephan (Herausgeber:in) / Wei, Zhenyu (Autor:in) / Ma, Lin (Autor:in) / Wang, Kexin (Autor:in) / Shao, Zhijiang (Autor:in)


    Erscheinungsdatum :

    16.04.2023


    Format / Umfang :

    24 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






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