Based on the analysis of the dynamic characteristics of a continuous thrust spacecraft, the variation of its orbit radius during orbital climb is studied, and the process of orbital climb is described in a formulaic manner, followed by identification of its thrust parameters. Firstly, describe the basic problem of orbital climb, analyze the spatial coordinate system and radar visibility characteristics; Secondly, formula derivation was carried out, and the transformation between spatial coordinate systems and the McLaughlin expansion of orbit radius were carried out; Finally, experimental simulations were designed to verify the accuracy of the proposed thrust parameter identification method. Using the LM algorithm, the solution accuracy can reach 1.5%.


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    Titel :

    Thrust Parameter Identification for Orbital Climbing of Continuous Thrust Spacecraft


    Beteiligte:
    Zhao, Shuailong (Autor:in) / Zhang, Yasheng (Autor:in) / Wang, Yaru (Autor:in)


    Erscheinungsdatum :

    19.05.2023


    Format / Umfang :

    4858275 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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