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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    Title :

    Thrust Parameter Identification for Orbital Climbing of Continuous Thrust Spacecraft


    Contributors:


    Publication date :

    2023-05-19


    Size :

    4858275 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English





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