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].


    Access

    Download


    Export, share and cite



    Title :

    Simultaneous Trajectory Optimization for Adaptive Powered Descent


    Additional title:

    Springer ser. in Astrophysics & Cosmology


    Contributors:
    Song, Zhengyu (editor) / Zhao, Dangjun (editor) / Theil, Stephan (editor) / Wei, Zhenyu (author) / Ma, Lin (author) / Wang, Kexin (author) / Shao, Zhijiang (author)


    Publication date :

    2023-04-16


    Size :

    24 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English






    Robust Trajectory Optimization for Guided Powered Descent and Landing

    Grace E Calkins / David C Woffinden / Zachary R Putnam | NTRS


    Robust Trajectory Optimization for Guided Powered Descent and Landing

    G. E. Calkins / D. C. Woffinden / Z. R. Putnam | NTIS | 2022