In the traditional development process of the launch vehicle guidance system, the system is designed repeatedly in the earlier stage and the verification of the system is conducted in the later stage. This development mode may cause some problems, such as low design efficiency and high cost. In order to improve the shortcomings of the traditional development process, in this paper the MBSE (Model Based System Engineering) method is introduced in the design phase of the launch vehicle guidance system, and the MBSE-based design model is used to carry out system verification in real time. The application of this method greatly improves the design efficiency of the launch vehicle guidance system. The MBSE-based simulation model of the launch vehicle guidance system is established, the system perturbation guidance simulation is carried out, and the result is compared with the standard design trajectory to verify the correctness of the guidance system designed based on MBSE.


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    Titel :

    MBSE-Based Guidance System Simulation of Launch Vehicle


    Weitere Titelangaben:

    Lect.Notes Mechanical Engineering


    Beteiligte:
    Rui, Xiaoting (Herausgeber:in) / Liu, Caishan (Herausgeber:in) / Ma, Guowei (Autor:in) / Wang, Qingtao (Autor:in) / Zhang, Wenfeng (Autor:in) / Yu, Rendong (Autor:in) / Liu, Xiong (Autor:in)

    Kongress:

    International Conference on Mechanical System Dynamics ; 2023 ; Beijing, China September 01, 2023 - September 05, 2023



    Erscheinungsdatum :

    18.06.2024


    Format / Umfang :

    12 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch