A new type of navigation system that meets the navigation requirements of deep space exploration missions with strong autonomous operation capability has become an urgent need. This paper proposes a new type of navigation constellation which has the characteristics of long-term stability under the full force model. Previously, we have studied that the orbits of the navigation constellation can be determined autonomously using the inter-satellite range data. As a continuation of the previous study, this article mainly studies the autonomous navigation performance of the navigation constellation under the actual force model. Here, the lunar probe’s mission of the Earth-Moon transition section is taken as an example, the observation data is inter-satellite ranging. When the ranging error is 1 m, the navigation constellation realizes autonomous navigation of the earth-moon transition section detector, and the navigation accuracy is within 1 m. The accuracy requirements are met. The current study can be used when deploying the navigation constellation in the Earth-Moon system.


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    Titel :

    Autonomous Navigation Based on Dynamical Substitutes in the Earth-Moon System Under the Full Force Model


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Yan, Liang (Herausgeber:in) / Duan, Haibin (Herausgeber:in) / Deng, Yimin (Herausgeber:in) / Liu, Bin (Autor:in) / Fang, Yanan (Autor:in) / Wang, Chong (Autor:in) / Zhang, Zhibin (Autor:in) / Wang, Jingyan (Autor:in)

    Kongress:

    International Conference on Guidance, Navigation and Control ; 2022 ; Harbin, China August 05, 2022 - August 07, 2022



    Erscheinungsdatum :

    2023-01-31


    Format / Umfang :

    7 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch